N318TZ, cancelled Aug 29, 2008
Service difficulty reports · 51
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 = 'N318TZ' AND deregistration_id = 'N318TZ-2008-08-29' 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 = 'N318TZ' AND deregistration_id = 'N318TZ-2008-08-29' 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 2008FA0000402Floorbeam · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON AFT CABIN FLOORBEAM, BS947, RBL 5 TO LBL5. S/O 245009, N/R 26378 (K)SDR 2008FA0000394Floor Support · corroded(REF DU4R2008220) DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOOR SUPPORT CABIN. STA 340, LBL 11. (K)SDR 2008FA0000391Floor Support · corroded(REF DU4R2008219) DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOOR SUPPORT CABIN STA 344, BL-0 TO BL-12L. (K)SDR AMTA200800051Hmu · activatedON PUSH BACK AND START OF NR 2 ENGINE, ENGINE CONTROL LIGHT ON. REPLACED NR 2 HMU IAW MM 73-21-10-4. OPS CHECKS NORMAL. (K)SDR AMAT200800050Eec · malfunctionedAFTER ENG NR2 WAS STARTED WE GOT AN ENGINE CONTROL LIGHT CAME ON. NR 2 EEC BITE SHOWED FAULT CODE 75-20582 TBV DEMAND AND SIGNAL DISAGREE. NO FAULTS ON CDS BITE. PERFORMED TEST 12 IAW MM 71-00-00-700-807. BOTH CHANNELS PASSED. NO FAULTS ON EEC. VERIFIED SDR AMTA200800029Radar · malfunctionedRADAR TILT INOPERATIVE CONTOUR LINES STAY AT 7 MILES. PERFORMED WEATHER RADAR RECEIVER/TRANSMITTER BITE TEST IAW FIM 34-43-00-81-801, NO DEFECT NOTED, OK FOR SERVICE. (K)SDR AMTA200700588Wheel · unserviceableAT 130 KTS, HEARD A POPPING NOISE AND AIRCRAFT STARTED PULLING TO THE RT, REJECTED TAKEOFF. FOUND NR 3 MLG TIRE TREAD SEPARATED. REMOVED AND REPLACED NR 3 MLG WHEEL ASSY IAW 32-45-11-4 AMM, NO DEFECTS NOTED. (K)SDR AMTA200700569Fmc · failedDUAL FMC FAILURE AT CRUISE ALTITUDE, LOST ALL STORED DARA, NAV DISPLAY RESTORED ITSELF AND FLIGHT CREW REPROGRAMMED FMC DATA. PERFORMED FMC SYSTEM BITE CHECK IAW 34-61-00-810-801, NO FAULTS NOTED ON FMC NR 1 AND NR 2 SYS OPS OK. (K)SDR AMTA200700460Connector · disconnectedRT FWD EMERGENCY EXIT LIGHTING INOPERATIVE. FOUND CONNECTING PLUG FOR BATTERY DISCONECTED REINSTALLED. OPS CK NORMAL IAW 33-51-06-2. (K)SDR AMTA200700462Duct · missingLT PACK ILLUMINATED DURING CLIMB PACK RESET BUT ILLUMINATED AGAIN TEMP WAS ABOUT 185. FOUND DISCHARGE DUCT TO ACM MISSING COUPLING, SECURED DUCT AND INSTALLED NEW COUPLING, LEAK CHECK GOOD, OPERATED PACK, TEMP 60 DEGREES NORMAL, PERFORMED BITE IAW FIM 21-62-0SDR AMTA200700442Battery Pack · inoperativeEMERGENCY LIGHTS (INTERIOR) BY 1L DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. IAW AMM 33-51-06-960-805. OPS CHECK GOOD. (K)SDR AMTA200700426Acm · unserviceableLT PACK TRIPPED IN FLT RESET IAW TO CHECK LIST, PACK TRIPPED AGAIN. INSPECTED, REMOVED AND REPLACED DEFECTIVE ACM IAW AMM 21-51-04. GROUND OPS CHECK GOOD. LT PACK, OK FOR SERVICE. (K)SDR AMTA200700314Valve · unserviceableGAT RETURN, DUE TO RT PACK LT ON, WOULD NOT RESET IAW QRH. REMOVED AND REPLACED PACK TEMPERATURE CONTROL VALVE IAW AMM 21-51-10-4. OPS AND LEAK CHECK GOOD. (K)SDR AMTA200700295Unknown · unknownFWD OVERWING AND AFT OVERWING DOOR LIGHT CAME ON, ON TAKEOFF. FOUND LT FWD OVERWING FLT LOCK BREAKER POPPED. RESET C/B. PERFORMED FIM TASK 52-20-00-810-801. SYSTEM TEST NORMAL OVERWING EXIT LIGHTS OUT. (K)SDR AMTA200700213Starter Gen · malfunctionedAPU WILL NOT START. REPLACED STARTER GENERATOR. OPS CHECK NORMAL. (K)SDR AMTA200700212Cdu · malfunctionedCAPTAIN`S CDU DISPLAY BLANK. REMOVED AND REPLACED CAPTAINS CDU REF 34-61-01. OPS CHECK GOOD. (K)SDR AMTA200700211Starter Gen · inoperativeAPU GEN INOPERATIVE. REMOVED AND REPLACED APU GEN OPS CHECK GOOD IAW 49-41-21-4. (K)SDR AMTA200700198Warning System · malfunctionedAPU FAULT LT ILLUMINATED ON START. PERFORMED APU BITE CK, FOUND MSG 49-41011, PERFORMED BITE CK IAW FIM 49-40-00-810, FIM 49-60-00-810, NO CURRENT FAULT FOUND. (K)SDR AMTA200700172Warning Light · illuminatedATTEMPTED START OF APU, FAULT LIGHT, NO LIGHT OFF. PERFORMED BITE IAW FIM 49-60-00-810-801-802, CURRENT FAULTS DISPLAYED. (K)SDR AMTA200700136Circuit Breaker · trippedINFLIGHT, FOUND WINDOW HEAT CB POPED FOR L2-L3-L4. ON P6-11 PANEL. PERFORMED BITE CK IAW FIM 30-40-00-810-801. RESET CIRCUIT BREAKER, OPS CK NORMAL. (K)SDR AMTA200700040Computer · malfunctionedL FMC FAILED AFTER ETP. INSPECTED AND OPS CHECK PER AMM 34-61-00. NO FAULT NOTED. (M)SDR AMTA200600687Skin · damagedLT IB FLAP HAS DAMAGE TO BULLNOSE AND LWR SURFACE PANEL AND 2 EA ENCERNTRIC BUSHINGS, ITEMS REMOVED FROM ONE AC TO THIS AC AND NEED TO BE REPAIRED IAW COMPANY. REPAIRED IAW EA, SRM. (K)SDR AMTA200600684Unknown · malfunctionedCONT CABIN ZONE TEMP LIGHT ILLUMINATED DURING CRUISE FLIGHT. WOULD NOT RESET. T/S IAW FIM 21-62-00-810-839. LIGHT DID NOT COME ON. OPS CK NORMAL. (K)SDR AMTA200600621Skin · gougedGOUGE ON EXT FUSELAGE SKIN JUST AFT OF L-1 DOOR LOWER AFT CORNER STATION 348.2. REMOVED DAMAGE, ORIGINAL MATERIAL THICKNESS .071, MATERIAL REMOVED 018, IAW 53-10-01-0I. TWO FASTENERS REMOVED AND REPLACED PER EA 737-5310-09-A0441. PRIMED AND PAINTED IAW MM 5SDR AMTA200600607Idg · malfunctionedLOSS OF NR 2 GENERATOR. REMOVED AND REPLACED NR 2 ENG IDG PER MM 24-11-11. OPS CHECK GOOD. (M)SDR AMTA200600580Attach Fitting · galledFOUND LEFT HORIZ STAB AFT ATTACH LOWER PIN GALLING. REPLACED LEFT HORIZ STAB ATTACH PIN NR 18041612-4. (M)SDR AMTA200600589Attach Fitting · galledFOUND RIGHT HORIZONTAL STABILIZER AFT ATTACH UPPER PIN GALLING AND CORROSION. REPLACED RIGHT HORIZONTAL STABILIZER AFT ATTACH PIN WITH P/N 180A1612-3. (M)SDR AMTA200600588Attach Fitting · corrodedRIGHT HORIZONTAL STABILIZER AFT ATTACH MIDDLE PIN HAD GALLING AND CORROSION. REPLACED RIGHT HORIZONTAL STABILIZER AFT MIDDLE ATTACH PIN WITH P/N 180A1612-4. (M)SDR AMTA200600587Attach Fitting · galledFOUND RIGHT HORIZONTAL STABILIZER AFT ATTACH BOTTOM PIN HAS GALLING AND CORROSION. REPLACED HORIZONTAL STABILIZER AFT ATTACH BOTTOM PIN WITH P/N 180A1612-4. (M)SDR AMTA200600586Attach Fitting · galledFOUND RIGHT HORIZONTAL STABILIZER FORWARD ATTACH LOWER BOLT GALLING AND CORROSION. REPLACED RIGHT HORIZONTAL STABILIZER FORWARD ATTACH LOWER BOLT WITH P/N 180A1611-3. (M)SDR AMTA200600581Attach Fitting · corrodedFOUND LEFT HORIZ STABILIZER AFT ATTACH PIN HAS CORROSION. REPLACED LEFT HORIZ STAB PIN P/N 180A1612-4. (M)SDR AMTA200600584Bolt · corrodedLEFT HORIZ STAB FORWARD ATTACH LOWER BOLT HAS CORROSION. REPLACED LEFT HORIZ FORWARD ATTACH LOWER BOLT WITH P/N 1804164-3. (M)SDR AMTA200600582Attach Fitting · galledLEFT HORIZ STABILIZER AFT ATTACH UPPER PIN GALLING. REPLACED LEFT HORIZ STAB AFT ATTACH PIN WITH P/N 180A1612-3. (M)SDR AMTA200600574Floor Panel · corrodedFOUND FORWARD CARGO FLOOR PANEL 2ND FROM AFT HAS CORROSION ON UPPER SURFACE STATION 500 TO 500D. FABRICATED FLOOR PANEL AS PER SRM 53-30-53-01. (M)SDR AMTA200600573Doubler · corrodedFOUND CORROSION ON AFT CARGO FLOORBOARD TO SIDE WALL RETAINING DOUBLER UNDERSIDE STATION 740. REMOVED CORROSION ON CAP STRIP, RETAINING DOUBLER, ACTUAL SIZE 42 INCH MAX ALLOWED 12.6 INCH AREA. REMOVED IS 4 SQUARE INCHES, FOUND TO BE WITHIN LIMITS PER 532-00-SDR AMTA200600535Battery · inoperativeA/C LEFT EMERGENCY BATTERY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY CHECK GOOD. (M)SDR AMTA200600585Attach Fitting · galledFOUND RT HORIZONTAL STAB FORWARD ATTACH UPPER BOLT GALLING AND CORROSION. REPLACED RT HORIZONTAL STAB FORWARD ATTACH UPPER BOLT WITH P/N 18A1611-3. (M)SDR AMTA200600583Attach Fitting · corrodedLT HORIZ STABILIZER FORWARD ATTACH BOLT HAS CORROSION. REPLACED LEFT HORIZ STABILIZER BOLT WITH 180A1611-3. (M)SDR AMTA200600506Iru · unserviceableIRS FAULT LIGHT ON FLT (LT). REMOVED AND REPLACED NEW ADIRU IAW MM, PERFORMED INSTALLATION TEST IAW MM, OK FOR SERVICE. (K)SDR AMTA200600452Monitor · failedFMC (R), FMC LT IRS MONITER BLANK ON ARRIVAL. POWER LT, RT FMC`S DOWN REINITIATED POWER SYS. OPS NORMAL. PERFORMED FMC BITE REF FIM. NO FAULTS FOUND. OK FOR SERVICE. (K)SDR AMTA200600450Regulator · unserviceableENG DUCT PRESSURE SPLIT. REMOVED AND REPLACED BLEED AIR REGULATOR ON NR 2 ENGINE, OPS CHECKED NORMAL IAW MM. (K)SDR AMTA200600446Shutoff Valve · unserviceableRT DUCT PRESSURE = 20 PSI, LT DUCT PRESSURE= 40 PSI BOTH IN CLIMP AND CRUISE. REMOVED AND REPLACED PRSOV VALVE AND OPS CHECKED NORMAL IAW MM. A/C OK FOR SERVICE. (K)SDR AMTA200600405Valve · malfunctionedLT AND RT DUCT PRESSURE POINTERS SPLIT WITH ENG BLEED ON, APU BLEED OFF. N1 89.0 EACH SIDE LT 40 PSI, RT 30 PSI FL370 WITH WING A/I ON BOTH LT AND RT = 28 PSI. T/S IAW FIM 361000810804 FOUND HIGH STAGE VALVE IAW MM. (K)SDR AMTA200600260Strip · separatedFWD FLOOR EGRESS STRIP AT 14D IS COMING APART. RESECURED EGRESS FLOOR STRIP 14D. (K)SDR AMTA200600187Filter · unknownAPU INOPERATIVE. REMOVED AND REPLACED NEW LUBE AND SCAVENGE FLTR IAW MM. RAN APU FOR 45 MINUTES IAW MM, NO DEFECT NOTED. (K)SDR AMTA200600144Fmc · malfunctionedCAPTAIN FMC LOCKED UP. REMOVED AND REPLACED CAPTAINS FMC CDU IAW AMM. OPS CHECK GOOD. (K)SDR AMTA200600139Line · looseRT DUCT PRESSURE DROPS FROM 35 PSI TO 15 PSI SERVER AT TIMES IN FLIGHT. FOUND LOOSE SENSE AIR LINE ON BLEED AIR REGULATOR. TIGHTENED LINE. PERFORMED FIM 36-10-00 810-807 OPS CHECK NORMAL. RAN ENG AT 80 PERCENT FOR 5 MINUTES, NO FLUCTUATIONS. (K)SDR AMTA200600126Transceiver · unserviceableRADAR HAS SMALL RETURNS CLOSE IN LESS THAN 3NM CONTINOUSLY. REMOVED AND REPLACED WEATHER RADAR RT OPS CHECK NORMAL REF 34-43-41-4. (M)SDR AMTA200400361Computer · malfunctionedELEVATORY FEEL DIFFERENTIAL LIGHT ILLUMINATED. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER IAW MM 27-31-37-4. COMPLIED WITH STEP 3G2 AND 3 MM 27-31-37-4 FEEL FORCE SYSTEM TEST AMM TASK 27-31-00-700-812. SYSTEM OPS CHECK GOOD. (M)SDR AMTA200300322Light · crackedFLOOR PATH LIGHTING RIGHT SIDE AFT END CRACKED. REMOVED AND REPLACED PATH LIGHT IAW MM 33-51-15-2.
Back to N318TZ, cancelled Aug 29, 2008