N29UA, cancelled Jan 18, 2018
Service difficulty reports · 68
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 = 'N29UA' AND deregistration_id = 'N29UA-2018-01-18' 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 = 'N29UA' AND deregistration_id = 'N29UA-2018-01-18' 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 ARWA20030908Spar Cap · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 4 PYLON LT LOWER SPAR CAP WITH CRACK STA YOP 251 BY ACCESS DOOR NR 411.SDR ARWA20030906Spar Cap · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 2 PYLON LT CENTER SPAR CAP WITH CRACK STA YIP 235.SDR ARWA20030905Angle · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 2 PYLON STUB WING BELOW LT SPAR CAP (Z) ANGLE WITH CRACK.SDR ARWA20030904Angle · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON STATION YIP NR 227 RT SIDE ANGLE WITH CRACK.SDR ARWA20030903Fitting · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON UPPER SECTION, FRONT SPAR AND FOOT STOOL SPLICE FITTING WITH 3 INCH CRACK.SDR ARWA20030902Web · crackedNR 188. DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 1 PYLON BETWEEN STATION YOP NR 226 AND STATION YOP NR 243 UPPER WEB DOUBLER WITH CRACKS. CORRECTIVE ACTION:SDR ARWA20030907Spar Cap · damagedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 4 PYLON INTERIOR STA YOP 225 LT LOWER SPAR CAP WITH STACK, BY ACCESS DOOR NR 426.SDR ARWA20030804Proximity Sensor · out of adjustDURING FINAL APPROACH, AFTER GEAR EXTENSION, NOSE LANDING GEAR LIGHT DID NOT ILLUMINATED. RETARDING POWER LEVERS CAN'T GET THE AURAL WARNING TO COME ON. EXECUTED GO-AROUND, DURING GO AROUND NOSE LANDING GEAR LIGHT STARTED TO FLICKER. VISUAL INSPECTION OF THSDR ARWA20030704Wire · chafedAFTER TAKE-OFF NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED ACCOMPLISHED APPROPRIATE CHECKLISTS, AND RETURNED TO SJU. REMOVED AND CHECKED NR 1 ENGINE MAIN OIL FILTER, FOUND OK. RE-INSTALLED FILTER, FOUND TWO WIRES WERE CHAFING WITH COWLING SPLICE AND RE-ROUTEDSDR ARWA20030604Line · leakingLOSS OF HYDRAULIC FLUID DOWN TO STAND-PIPE. LOSS OF HYDRAULIC CHECK LIST COMPLETED. INSPECTED NR 3 PYLON FOR EVIDENCE OF HYDRAULIC LEAK, FOUND RIGID LINE DAMAGED INSIDE PYLON AREA; REMOVED AND REPLACED RIGID LINE ASSEMBLY AS REQUIRED IAW MM 20-12-0; OPERATIOSDR ARWA20030504Line · leakingDURING CRUISE, LOST HYDRAULIC QUANTITY FOLLOWED THE LOSS OF HYDRAULIC FLUID OR PRESSURE. ABNORMAL OR EMERGENCY CHECKLIST. REMOVED AND REPLACED FLEX HYDRAULIC LINE ON NR 2 ENGINE PER MM 29-10-12. RUN UP CHECK ACCOMPLISHED AS PER MM 71-00-0 NO LEAK FOUND ITSDR ARWA20030209Smoke Detector · failedON PRE-FLIGHT, LOWER CARGO SMOKE DETECTOR MAINTENANCE LIGHT ON. ENTERED ON DMI 17527 IAW MEL 26-10-1-1A. REMOVED AND REPLACED LOWER SMOKE DETECTOR UNIT (SDU) FA 16037. OPERATIONAL CHECK IAW STC ST00746LA-D FOUND NORMAL. CLEARED DMI # 17527 AND REMOVED PLSDR ARWA20030208Smoke Detector · failedON PRE-FLIGHT FOUND FORWARD "A" BELLY LOWER CARGO SMOKE DETECTOR INOPERATIVE. ENTERED ITEM ON DMI 17493 AS PER MEL 2G-10-1-0-1 CAT "B". REMOVED AND REPLACED SMOKE DETECTOR UNITS (SDUS) S/N 4566, 14470 & 13067 AS PER STC ST00746LA-D. OPERATIONAL CHECK GOSDR ARWA20020915Hydraulic Line · leakingLOSS OF HYDRAULIC FLUID IN FLIGHT, PERFORMED EMERGENCY CHECKLIST AND LANDED IN MIA WITHOUT FURTHER INCIDENT. FOUND NR 2 ENGINE HYDRAULIC CASE DRAIN LINE LEAKING. REMOVED & REPLACED LINE IAW MM 20-12-0. SERVICED HYDRAULIC FLUID IAW MM 12-30-1, PREFORMED LEAKSDR ARWA20020702Indicator · malfunctionedON CLIMBOUT OF MIAMI AT 17,000 FEET F/O ARTIFICIAL HORIZON FAILED WITH ATTITUDE FLAG. RETURNED WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LANDING AT 273,000 LBS. WIRING CHECK ACCOMPLISHED IAW MM 34-2-2. REMOVED AND REPLACED 2 AMP C/B B10-58 AND NR 2 ADI AS PSDR ARWA20020701Gyro · failedAT START OF TAKEOFF ROLL F/O ARTIFICIAL HORIZON FAILED WITH FLAG, REJECTED TAKEOFF AT 40 KNOTS AND RETURNED TO RAMP. REMOVED AND REPLACED NR 2 VERTICAL GYRO IAW MM 34-25-0. GROUND TEST OK. AIRCRAFT RETURNED TO SERVICE.SDR ARWA20020603Bleed Valve · seizedENGINE NR 4 UNABLE TO SPOOL TO MAX POWER DURING TAKEOFF. REMOVED AND REPLACED ENGINE BLEED VALVE IAW MM 75-30-3; OPERATIONS CHECKED NORMAL IAW MM 71-00.SDR ARWA20020510Warning System · malfunctionedAT BEGINNING OF TAKEOFF, ROLL SPOILER EXTENDED, LIGHT ILLUMINATED. ABORTED TAKEOFF. PERFORMED VISUAL INSPECTION OF SPOILERS DEPLOY SWITCHES AND MECHANISM; CLEANED CONNECTOR TO MICRO-SWITCH PERFORMED OPERATIONAL CHECK IAW MM 27-61-0 AND 27-63-0. OPERATIONAL SDR ARWA20020506Hydraulic Line · leakingAT 2225Z IN CLIMBING, HYDRAULIC QUANTITY DROPPED TO STAND PIPE PRESSURE DROPPED TO ZERO RETURNED TO KMIA. PERFORMED LOSS HYDRAULIC PRESSURE EMERGENCY CHECKLIST ON HYDRAULIC FLUID; PERFORMED EMERGENCY CHECKLIST ON HYDRAULIC CHECK, NO FURTHER LOSS OF FLUID. USSDR ARWA20020312Proximity SwitchLOG PAGE # 108372. DISCREPANCY: GEAR NOT LATCHED, DOOR NOT LATCHED, LIGHTS ILLUMINATED. ON LEFT MAIN LANDING GEAR NO DOWN LIGHTS. CORRECTIVE ACTION: REMOVED AND INSTALLED LEFT MAIN GEAR PROXIMITY SWITCH SENSOR. ACCOMPLISHED ADJ & TEST POSITION & WARNING SYSDR ARWA20020205Spar · crackedDURING C-CHECK, LEFT WING STA XW 60 AUXILIARY SPAR LUG WITH CRACK, ADJACENT TO MLG TRUNNION FITTING. REMOVED AND REPLACED AUXILIARY SPAR IAW DRAWING 5616128.SDR ARWA20020109Gcu · failedDURING APPROACH NR 4 GENERATOR UNPARALLEL LIGHT AND BUS POWER FAIL LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST. AIRCRAFT LANDED AT DESTINATION UNEVENTFUL. RESET NR 4 GENERATOR SYSTEM IN ACCORDANCE WITH MM 24-5-1 ENTERED ON DMI 16156 PER MEL 24-1 GEN NR SDR ARWA20011216Filter Housing · defectiveNR 4 ENGINE OIL PRESSURE ERRATIC FLUCTUATES BETWEEN 0 TO 20 PSI WITH OIL PRESSURE LIGHT ON. ENGINE SHUTDOWN AS PER ABNORMAL CHECKLIST AND PROCEDURES. AIRCRAFT LANDED UNEVENTFUL. REMOVED AND REPLACED GEARBOX IAW MM 72-00. ACCOMPLISHED RUN UP, NO LEAKS NOTEDSDR ARWA20011214Transmitter · erraticNR 4 OIL PRESSURE WENT TO 0 PSI AFTER TOP OF DESCENT, NR 4 OIL PRESS LIGHT ILLUMINATED, ENGINE WAS SHUT DOWN. BLED NR 4 ENGINE OIL SYSTEM, REMOVED AND REPLACED MAIN OIL FILTER IAW P&W 72-0, FOUND OIL PRESS XMTR ERRATIC, R&R IAW MM 79-32-1, OPS CKD DURING ENGISDR ARWA20011203Brake · seizedNR 2 MAIN LANDING GEAR BRAKE ASSEMBLY LOCKED-UP CAUSING NR 2 TIRE TO BLOW. BRAKE TEMPERATURE CHECK AND WITHIN LIMITS. REMOVED AND REPLACED NR 2 MAIN GEAR BRAKE ASSEMBLY IAW DC-8 MM 32-42-1. REMOVED AND REPLACED NR 2 MAIN GEAR WHEEL AND TIRE ASSEMBLY IAW MM SDR ARWA20011104Hydraulic Line · leakingAFTER T/O LOST HYDRAULIC FLUID TO STAND PIPE AND PRESS 0, PERFORMED LOSS OF HYDRAULIC FLUID AND PRESS CHECKLIST AND RETURNED TO MIAMI. LANDED IN MIAMI OVERWEIGHT AT 272,600 WITHOUT INCIDENT. FOUND LT MLG BUNGEE CYLINDER PRESSURE LINE LEAKING. REMOVED AND RESDR ARWA0010805Stringer · crackedDURING SCHEDULED MAINTENANCE:FOUND 2 INCH CRACK AT STATION 940 STRINGER 23R.REPAIRED IAW EO DRAWING NR AS11300 DATED 08/09/01SDR ARWA0010804Stringer · crackedDURING SCHEDULED MAINTENANCE:FOUND 2 INCH CRACK AT STATION 940 STRINGER 23R.CORRECTIVE ACTION:REPAIRED I.A.W. E.O. DRAWING # AS11300 DATED 08/09/01SDR ARWA0010302Control Box · failedON GEAR DOWN HAD NO RIGHT MAIN GEAR GREEN LIGHT AND HAD GEAR NOT LATCHED AND DOOR NOT LATCHED RED LIGHTS ON. EMERGENCY CHECK LIST ACCOMPLISHED PLUS SEVERAL CYCLES. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED PROXIMITY SWITCH CONTROL BOX. INDICATION SYSTEMSDR ARWA0001202Door Latch · lack of lubeLANDING GEAR DOORS NOT LATCHED LIGHT ON AFTER GEAR RETRACTION - PERFORMED ABNORMAL CHECK-LIST CYCLED GEAR SEVERAL TIMES. PERFORMED OVERWEIGHT LANDING. CHECKED BOTH MLG DOOR UPLATCHES MECHANISM. BOTH FOUND NORMAL. CLEANED PROXIMITY SWITCHES AND LUBRICATED MECSDR 20000410AP004Light · inoperativeWHILE ON THE GROUND AT SAN JUAN, CREW REPORTED EMERGENCY LIGHTS FAILED TO DISARM TEST. RESET EMERGENCY LIGHT C/B, OPERATIONAL CHECK NORMAL IAW MM 33-50-2. (M)SDR 2000ZZZM228Fire Loop · looseNR 4 ENGINE FIRE WARNINGS CAME ON AFTER REACHING 3,000 FT FOLLOWED EMERGENCY CHECKLIST IAW FINE AIR POLICY. TROUBLESHOOT SYSTEM AND FOUD LOWER ENGINE FIRE LOOP LOOSE. RE-SECURED LOOP IAW MM 26-10-1. (M)SDR 2000ZZZX360Floorbeam · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE FLOORBEAM AT STA BS 920 APPROXIMATELY LBL 45. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5310-06:00, SEMAN EO NR 9908202.SDR 2000ZZZX354Panel · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RT WING CORRODED AT OUTER WING OUTBOARD OF EXTENDED LEADING EDGE AT STA XFS 710. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5754-01:00, SEMAN EO NR 990096 AND BOEING MESSAGE M-7200-99-08383 AND M-7200-9SDR 2000ZZZX353Panel · crackedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LT WING INNER AFT TOP PANEL PLATING CRACKED AND CORRODED AT STA XW 408 BETWEEN STRINGERS 2 AND 3. REPAIRED CRACK IN WING IAW FINE AIRLINES EA NR G5730-04:00, SEMAN EO NR 990095 AND BOEING MESSAGE M-7200-99-0779SDR 2000ZZZX352Skin · crackedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION AND CRACK ON LT WING INNER EXTENDED LEADING EDGE AT LOWER SKIN BETWEEN STA FS 304 TO XFS 341. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5730-03:00, SEMAN EO NR 990102 AND BOEING MESSAGE SEU-LSDR 2000ZZZX351Floorbeam · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE FLOORBEAM AT STA FS 1680. REPAIRED CORROSION DAMAGE IAW WITH FINE AIRLINES EA NR G5310-05:00, SEMAN EO 9908241.SDR 2000ZZZX350Panel · crackedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CRACK AND CORROSION ON LT WING INNER AFT PLATING PANEL AT STA XRS 69 AFT OF REAR SPAR. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5730-07:00, SEMAN EO NR 990101 AND BOEING MESSAGE M-7200-99-08151.SDR 2000ZZZX349Fitting · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON LT LONGERON 24 CORROSION DAMAGED AT STA 940 IN LR WHEELWELL. REPAIRED CORROSION DAMAGE IAW SRM 53-2-0.SDR 2000ZZZX348Longeron · crackedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LT LONGERON 24 CRACKED BETWEEN STA 960 AND STA 980 IN LT WHEELWELL. REPAIRED CRACK IAW FINE LINES EA NR G5313-12:00, SEMAN EO NR 990089 AND BOEING MESSAGE M-7200-99-06994.SDR 2000ZZZX347Spar · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON VERTICAL FIN ON LT AND RT REAR SPAR AT STA ZR 45. REPAIRED CORROSION DAMAGE IAW FINE LINES EA NR G5531-01:00, SEMAN EO NR 990092 AND BOEING MESSAGE M-7200-99-08438.SDR 2000ZZZX346Skin · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FUSELAGE TOP HAS CORROSION AT STA 940.000 AND BETWEEN LONGERONS L1 AND L2 RT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-09:00, SEMAN EO NR 990091 AND BOEING MESSAGE M-7200-99-07538.SDR 2000ZZZX345Skin · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FUSELAGE TOP HAS CORROSION DAMAGE AT STA 717 BETWEEN LONGERONS L1 TO L2, LT. REPAIRED CORROSION DAMAGE IAW WITH FINE AIRLINES EA NR G5313-10:00, SEMAN EO NR 990084 AND BOEING MESSAGE M-7200-99-08106.SDR 2000ZZZX344Skin · crackedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LT PASSENGER DOOR, LOWER AFT JAMB CORNER CRACKED. REPAIRED CRACK DOOR IAW FINE AIRLINES EA NR G5320-01:00; SEMAN EO NR 990082 AND BOEING MESSAGE M-7200-99-07463SDR 2000ZZZX343Skin · corrodedDURING C-CHECK INSPECTION, FOUND FOLLOWING: CORROSION ON FUSELAGE TOP AT STA 980, BETWEEN LONGERONS L2 LT AND L2 RT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-07: 00, SEMAN EO NR 990093 AND BOEING MESSAGE M-7200-99-07595.SDR 2000ZZZX342Fitting · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON RT LONGERON 24 CORROSION DAMAGED AT STA 960 IN RT WHEELWELL. REPAIRED CORROSION DAMAGE IAW SRM 53-20-0.SDR 2000ZZZX341Fitting · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON LT LONGERON 24 CORROSION DAMAGED AT STA 879.375 IN LT WHEELWELL. REPAIRED CORROSION DAMAGE IAW SRM 53-2-0.SDR 2000ZZZX340Fitting · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON LT LONGERON 24 CORROSION DAMAGED AT STA 960 IN LT WHEELWELL. REPAIRED CORORSION DAMAGE IAW SRM 53-2-0.SDR 2000ZZZX339Skin · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON FUSELAGE TOP AT STA 898 TO STA 911 BETWEEN LONGERONS L2 LT AND L4 RT. REPAIRED FUSELAGE CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-05:00, SEMAN EO 990099 AND BOEING MESSAGE SEU-LIM-99-00019H.SDR 2000ZZZX338Fitting · crackedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RIGHT MAIN LANDING GEAR TRAPEZOIDAL SUPPORT FITTING WITH FOUR CRACKS AT STA 868 IN RT WHEELWELL. REPAIRED CRACKS IAW SEMAN EO NR 9900990 AND BOEING MESSAGE M-72-00-99-06884. FINE AIRLINES EA NR G3211-01:00.
Back to N29UA, cancelled Jan 18, 2018