N128NA, cancelled Aug 17, 2009
Service difficulty reports · 49
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 = 'N128NA' AND deregistration_id = 'N128NA-2009-08-17' 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 = 'N128NA' AND deregistration_id = 'N128NA-2009-08-17' 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 PCSA2009021801Smoke Detector · dirtyCREW LOG ITEM, CARGO SMOKE LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT. BABY CHICKS WERE TRANSPORTED IN POSITIONS 3-7. MAINTENANCE CLEANED THE SMOKE DETECTORS FROM POSITION 2-7 AND THE SYSTEM TESTED NORMAL IAW THE MM. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR PCSA2009012801Smoke Detector · false activationCARGO SMOKE LIGHT ILLUMINATED DURING DESCENT. MX REPLACED NR1 AND NR3 SMOKE DETECTORS.SDR PCSA2009012701Smoke Warning · false activationCARGO SMOKE LIGHT ILLUMINATED IN FLIGHT, RAN ALL APPROPRIATE CHECKS, FALSE INDICATION, CONTINUED FLIGHT. MX PERFORMED AN OPS TEST OF THE SMOKE DETECTION SYS AND FOUND GOOD IAW THE MM.SDR PCSA2008121801Smoke Detector · dirtyON DESCENT, MAIN CABIN SMOKE DETECTOR LIGHT ILLUMINATED. NO EVIDENCE OF SMOKE DISCOVERED. MX DISCOVERED NR 1 SMOKE DETECTOR DIRTY. THE DETECTOR WAS CLEANED AND THE SYS TESTED NORMAL.SDR 2008040101Warning System · malfunctionedAMERIJET FLIGHT 8110 FROM TSSJ TO KMIA - MAIN CARGO COMPARTMENT SMOKE WARNING CAME ON IN CRUISE FLIGHT. VISUALLY CHECKED FALSE WARNING. ON ARRIVAL KMIA THE MAIN CARGO SMOKE DETECTION SYSTEM WAS OPERATIONALLY TESTED AND NO DEFECTS WERE FOUND.SDR C7WA200400082Switch · intermittentNR 2 KRUGER FLAP EXTEND LIGHT REMAINED ON AFTER TAKEOFF. REMOVED AND REPLACED NR 2 KRUGER FLAP SWITCH IAW MM.SDR C7WA200400037Skin · crackedFOUND FUSELAGE SKIN CRACKED STRINGER 21 LEFT STATION 1233. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 3. REPAIR DOUBLER, FABRICATED FROM 2024-T3, .080 BY 8 BY 7. (M)SDR C7WA200400034Hinge · crackedFOUND MAIN CARGO DOOR UPPER AFT HINGE SECTION CRACKED. REMOVED AND REPLACED UPPER AFT HINGE SECTION PER AEI SERVICE BULLETIN AE01-01 AND AEI MM CHAPTER 52 PAGE 15. (M)SDR C7WA200400035Skin · corrodedFOUND FUSELAGE SKIN CORRODED STRINGER 27 RIGHT STATION 500. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 6. REPAIR DOUBLER FABRICATED FRAME 2024-T3, .050 BY 31.25 BY 18. (M)SDR C7WA200400036Skin · corrodedFOUND FUSELAGE SKIN CORRODED STRINGER 17 LT STATION 1183. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 3A. REPAIR DOUBLER FABRICATED FROM 2024-T3, .080 BY 17 BY 11.80. (M)SDR C7WA200400033Pcu · leakingIN CRUISE NOTED DECREASING HYDRAULIC A-SYSTEM QUANTITY. FOLLOWED ABNORMAL PROCEDURES QUANTITY STABILIZED AT .6 GALLONS. FOUND LT ELEVATOR POWER CONTROL UNIT LEAKING. REMOVED AND REPLACED LT ELEVATOR PCU IAW MM. OPS AND LEAK CHECK GOOD.SDR C7WA200400049Pcu · leakingIN CRUISE NOTED DECREASING HYDRAULIC A-SYSTEM QUANTITY. FOLLOWED ABNORMAL PROCEDURES QUANTITY STABILIZED AT .6 GALLONS. FOUND LEFT ELEVATOR POWER CONTROL UNIT LEAKING. REMOVED AND REPLACED LEFT ELEVATOR PCU IAW B727 MM 27-30-81, OPS AND LEAK CHECK GOOD. (MSDR C7WA200300049Pin · brokenREJECTED TAKEOFF, NR 3 EPR UNRELIABLE AT TAKEOFF POWER READS LOW. SEEMS TO READ NORMAL AT CRUISE POWER. FOUND WIRE NOT CONNECTED TO PIN NR 3 AT EPR GAUGE CANNON PLUG. INSTALLED NEW PIN AND RECONNECTED WIRE IAW WIRING STANDARD PRACTICE CH 20 EPR READS NORMALSDR C7WA200200042Line · leakingLOST SYSTEM A HYDRAULIC. ENGINE NR 1 PUMP LOW PRESSURE LIGHT FOLLOWED BY FLUID LOSS IN FLIGHT. REMOVED AND REPLACED TWO EACH HYDRAULIC LINES, P/N 65-17844-250 AND 65-17844-17, LEAK CHECK GOOD. (M)SDR C7WA200200041Control Panel · shortedWHEN ENGAGING AUTOPILOT, CRUISE STABILIZER TRIMS TO THE FULL NOSE DOWN POSITION. WITH AUTOPILOT DISCONNECTED, AFTER LEVEL OFF AT FL350, AN ELECTRICAL OVERHEAT ODOR STARTED TO FILL THE COCKPIT. CHECKLIST PERFORMED, ODOR STOPPED. REMOVED AND REPLACED RIGHT ELSDR C7WA200200031Connector · brokenDURING FLIGHT, THE NR 1 ALTIMETER FLAG CAME IN VIEW AND STAYED. DIVERTED FLIGHT TO YIP. FOUND PIN 16 ON TOP PLUG OF AIR DATA COMPUTER BROKE. REPAIRED WIRE IAW MM CHAPTER 20. PERFORMED BITE TEST IAW MM 34-12-0 IAW BOEING MM 34-12-0. REF C7WA200200030 - AIRSDR C7WA200200030Adc · failedAIRCRAFT DEPARTED YIP AT 23:52Z AND HAD AIR DATA INSTRUMENT FAILURE CLIMBING THRU 5000FT. AIRCRAFT RETURNED TO YIP AND MADE OVERWEIGHT LANDING.SDR C7WA20020029Pitot Tube · obstructedREJECTED TAKEOFF FROM SJC AT 90 KNOTS DUE TO LACK OF AIRSPEED INDICATION ON COPILOTS SIDE. CHECKED PITOT TUBES AND FOUND INSPECT BLOCKAGE FROM FIRST OFFICERS PITOT TUBE. REMOVED BLOCKAGE CHECKED SYSTEM IAW MM 34-11-31. (M)SDR C7WA200200029Pitot Tube · obstructedREJECTED TAKEOFF FROM SJC AT 90 KNOTS DUE TO LACK OF AIRSPEED INDICATION ON COPILOTS SIDE. CHECKED PITOT TUBES AND REMOVED INSECT BLOCKAGE FROM F/O PITOT SYSTEM IAW MM 34-11-31.SDR COOSDR020214Structure · delaminatedRIGHT WING, OUTBOARD AILERON TRAILING EDGE (PN 65-21766-66)(SN BN-26) WITH DELAMINATION.SDR COOSDR020210Skin · corrodedLEFT WING, OUTBOARD AFT FLAP (PN 65-21635-85) (SN BN120) UPPER SKIN AND HONEYCOMB CORE SECTION CORRODED.SDR COOSDR020209Skin · delaminatedLEFT WING SPOILER NR 7 (PN 65-17348-74) (SN 7888K) LOWER SKIN WITH DELAMINATION.SDR COOSDR020208Skin · delaminatedRIGHT WING SPOILER NR 9 (PN 65-17348-74) (SN 9087K) LOWER SKIN WITH DELAMINATION.SDR COOSDR020207Structure · delaminatedLEFT WING, OUTBOARD AILERON TAB (PN 65-21726-33) TMC 189 WITH DELAMINATION.SDR COOSDR020206Skin · corrodedLEFT WING, INBOARD AFT FLAP (PN 65-21634-79)(SN BN147) UPPER, LOWER SKIN AND HONEYCOMB CORE CORRODED.SDR COOSDR02205Skin · delaminatedLEFT WING, SPOILER NR 5, (PN 65-17348-75), (SN 1781P) WITH DELAMINATION AT UPPER SKIN AND LOWER SKIN.SDR COOSDR02204Skin · delaminatedLEFT WING, SPOILER NR 4, (PN 65-17347-42), (SN TC-248) WITH DELAMINATION AT UPPER SKIN.SDR COOSDR020203Panel · delaminatedRIGHT WING, TRAINLING EDGE - LOWER FIX PANEL (PN 65216522) DELAMINATED.SDR COOSDR020202Structure · corrodedRIGHT WING, INBOARD AFT FLAP (PN 65-21634-92) (SN BN480) UPPER, LOWER SKIN AND HONEYCOMB CORE CORRODED.SDR COOSDR02200Panel · delaminatedRIGHT WING, TRAILING EDGE - LOWER PANEL (PN 6521652616) DELAMINATED.SDR COOSDR02197Panel · delaminatedRIGHT WING, TRAILING EDGE-UPPER PANEL (PN 6521657242) DELAMINATED.SDR COOSDR02196Structure · delaminatedRIGHT WING, SPOILER NR 14, (PN 651734757), SN 9126S WITH DELAMINATION.SDR COOSDR02195Structure · delaminatedRIGHT WING, SPOILER NR 8 (PN 651734866A) WITH DELAMINATION.SDR COOSDR02194Structure · delaminatedRIGHT WING, SPOILER NR 10, PN 65-17348-75, SN 4268H WITH DELAMINATION.SDR COOSDR02193Angle · crackedMAIN CARGO DOOR (PER STC NO SA1797SO) UPPER JAMB, FORWARD AND AFT CORNER ANGLE CRACKED.SDR 2000ZZZM63Nr 3 Disk · failedFLT 312 - KCLT-KMIA - AFTER TAKEOFF EPR DECREASED AND EGT INCREASED. RETARDED THROTTLE TO CONTROL EGT WHEN VIBRATION WAS NOTICED AND EXPERIENCED COMPRESSOR STALL. WHEN THROTTLE RETURNED TO IDLE, EGT CONTINUED TO CLIMB. PERFORMED ENGINE INFLIGHT SHUTDOWN PROSDR 98ZZZM5Air Distribution · odorFLT 230 - DTW-LRD - FLIGHT DIVERTED TO HDY, STRONG SMELL OF ELECTRICAL SMOKE. NO VISIBLE SMOKE, SEEMED TO BE AROUND FE PANEL. INSPECTED FE PANEL AND ADJACENT AREAS, P-6 PANEL, STAB TRIM C/B FOR ABNORMAL SMELL AND EXCESSIVELY HOT COMPONENTS. NONE FOUND. INSSDR C8GA977103Engine · failedFLT 224 - KPAP-KMIA - ON TAKEOFF ROLL, AT APPROXIMATELY 65 KTS, ENGINE NR 2 FAILED. WITH PRONOUNCED VIBRATION IN POWER QUADRANT AND ENGINE FAIL LIGHT ILLUMINATED. ENGINE READINGS, EPR 0, N1 22 PERCENT, N2 45 PERCENT, FF 1200, EGT 570 DEGREES. (M)SDR 96ZZZX6181Fuel Control · failedFLT PT 301 DEPARTED MIAMI, FL FOR CUARAZAO (CUR) ON THIS DATE. TAKEOFF WAS NORMAL UP TO THE TIME OF THE FIRST POWER REDUCTION. POWER REDUCTION WAS NORMAL FOR NR 2 AND NR 3 ENGINES; BUT, NR 1 ENGINE REMAINED AT HI POWER WITH NO RESPONSE TO THROTTLE MOVEMENT. SDR 96ZZZX6148Downlock Switch · inoperativeAFTER TAKEOFF FROM TPA WITH THE GEAR HANDLE IN THE GEAR UP POSITION, BOTH THE RED AND GREEN NOSE GEAR LIGHTS REMAINED ILLUMINATED. THE GEAR HANDLE WAS PLACED IN THE GEAR DOWN POSITION AND THE AIRCRAFT RETURNED TO TPA WITHOUT INCIDENT. TROUBLESHOOTING OF THE SDR 96ZZZX5201Pitot Tube · blockedMIAMI - ON TAKEOFF ROLL, THERE WAS NO AIRSPEED INDICATION ON THE CAPTAIN'S AIRSPEED INDICATOR. DISCONNECTED PITOT PRESSURE LINE, APPLIED NITROGEN PRESSURE AND FOUND INSECTS (BEES) CLOGGING CAPTAIN'S PITOT TUBE. CLEARED AL INSECTS FROM CAPTAIN'S PITOT LINES, SDR 95ZZZZ274Stringer · corrodedIN THE PROCESS OF COMPLYING WITH S/B 53-159 BELLY SKIN REPLACEMENT, STRINGER (P/N 65-56441-8) WAS FOUND CORRODED ALONG TOPSIDE. STRINGER WAS REPLACED.SDR 95ZZZX4159Stringer · corrodedIN THE PROCESS OF COMPLYING WITH SB 53-159 BELLY SKIN REPLACEMENT, SOME CORROSION WAS FOUND ON LEFT SIDE OF STRINGER PN 65-56129-10. THE STRINGER HAD TO BE REPLACED. THIS STRINGER RUNS ALONG THE LOWER END OF NR 2 CARGO DOOR. SUBMITTER STATED CAUSE OF THIS CSDR 95ZZZX4158Stringer · corrodedIN THE PROCESS OF COMPLYING WITH SB 53-159, BELLY SKIN REPLACEMENT STRINGER P/N 65-56441-8 WAS FOUND CORRODED ALONG TOP SIDE. STRINGER WAS REPAIRED. SUBMITTER STATED CAUSE OF CORROSION WAS EITHER MOISTURE BUILD-UP OR LACK OF FINISH ON THE PART.SDR 95ZZZZ273Stringer · crackedIN THE PROCESS OF COMPLYING WITH S/B 53-159 BELLY SKIN REPLACEMENT STRINGER (P/N 65-56441 WAS FOUND TO BE CRACKED AT BOLT HOLES FWD END OF STRINGER.SDR 95ZZZZ270Stringer · crackedIN THE PROCESS OF COMPLYING WITH SB 53-159 BELLY SKIN REPLACEMENT, STRINGER (P/N 65-56441-7) WAS FOUND TO BE CRACKED AT BOLT HOLES FWD END OF STRINGER.SDR 95ZZZX4162Blkhd Web · corrodedDURING A C-CHECK INSPECTION, CORROSION WAS FOUND AT STA 351.2 FORWARD BULKHEAD WEB SHEAR TIE AND ADJACENT AREA. AS THE CORROSION WAS FOUND IN NUMEROUS AREAS, THE BULKHEAD WEB WAS REPLACED. THE REPAIR WAS ACCOMPLISHED WITH THE HELP OF BOEING AIRCRAFT COMPANY.SDR 95ZZZX4160Structure · corrodedDURING A C-CHECK INSPECTION, FOUND SEVERAL STRINGERS AND DOUBLERS CORRODED IN LOWER BELLY AREA FROM STA 320 - STA 360. INTERNAL DOUBLER CORRODED ON SKIN PANEL STA 351 TO STA 360, STR 27L TO STR 27R. STRINGER SEGMENT CORRODED STA 351 TO STR 360, STR 26R. FRAMSDR 95ZZZZ271Stringer · crackedIN THE PROCESS OF COMPLYING WITH S/B 53-159 BELLY SKIN REPLACEMENT, CHORD STRINGER (P/N 65-56441-7) WAS FOUND TO BE CRACKED AT FWD BOLT HOLES. THE ED IN THAT AREA SEEMS TO BE MARGINAL.
Back to N128NA, cancelled Aug 17, 2009