N784AL, cancelled Feb 16, 2017
Service difficulty reports · 73
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 = 'N784AL' AND deregistration_id = 'N784AL-2017-02-16' 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 = 'N784AL' AND deregistration_id = 'N784AL-2017-02-16' 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 22AA20090505Spar · crackedON PRE FLIGHT FOUND FUEL LEAK BY LEFT WING ROOT FORWARD OF WHEEL WELL. UPON FURTHER INVESTIGATION THE LEFT REAR SPAR WAS FOUND CRACKED.SDR 22AA20081203Bleed Valve · stuckLOG PAGE NR 128276. NR 1 ENGINE WOULD NOT ACCELERATE TO TAKE-OFF POWER; REJECTED TAKE OFF AT 80 KTS. - RETURNED TO GATE. FOUND NR 1 COMPRESSOR BLEED VALVE STUCK IN OPEN POSITION. R&R NR 1 ENGINE COMP. BLEED CONTROL VALVE IAW DC-8 M/M 75-30-3; OPS CHECK NORSDR 22AA20081102Control Cable · brokenON DESCENT LONG TRIM SUITCASE HANDLE, RIGHT SUITCASE HANDLE JAMMED. FOUND BROKEN CABLE RUNNING NR 49B. REMOVED AND REPLACED 1/16 CONTROL CABLE RUNNING NR 49B IN ACCORDING WITH DC-8 MAINTENANCE MANUAL 27-40-01. RIGGING AND OPERATION CHECKED, FOUND NORMAL IN SDR 22AA20081002Cylinder · malfunctionedON APPROACH INTO MROC THE FLAPS WOULD NOT EXTEND BEHOND 23 DEGREES. FOUND OUTBOARD FLAP LOCKOUT CYLINDER RETRACTED; SERVICE FLAP LOCKOUT CYLINDERS IAW MM 27-51-10. OPERATIONAL CHECK FOUND NORMAL IAW MM 27-50-00.SDR ARWA20080802Unknown · sparksAIR TURNBACK REPORTED SPARKS COMING FROM RT MAIN GEAR. DECLARED EMERGENCY AND RETURNED TO MIA. (S)SDR ARWA20080201Limit Switch · malfunctionedDURING TAKEOFF ROLL, TAKEOFF WARNING HORN CAME ON. REMOVED AND REPLACED SI-278 FLAP UPLIMIT SWITCH IN ACCORDANCE WITH M/N 27-52-1 AND SI-177 AND 176 SPOILERS SWITCH IN ACCORDANCE WITH 27-63-1, SYSTEM GROUND TEST NORMAL.SDR ARWA20071205Snap Ring · looseDURING CLIMB-OUT, UNABLE TO CONTROL THE CABIN PRESSURIZATION, NEITHER WITH AUTO OR MANUAL (WITH 4 T.C. ON). FOUND NR 2 TC DISFUSER SNAP RING LOOSE. REINSTALLED SNAP RING AT NR 2 TC IN ACCORDANCE WITH DC-8 M/M 21-10-6. PRESSURIZATION CHECK FOUND NORMAL IN ACSDR ARWA20061005Bellcrank · brokenON POST FLIGHT FOUND NOSE GEAR DOOR BROKEN LINK. REMOVED TORQUE TUBE AND BELL CRANK IN ACCORDANCE WITH M/M 32-22-2. INSTALLED BELL CRANK AND REINSTALLED NOSE GEAR DOOR LINKAGE IN ACCORDANCE WITH M/M 32-33-2; OPERATIONAL CHECK IN ACCORDANCE WITH M/M 32-22-1 ASDR ARWA20061004Wire · damagedLOST ALL HYDRAULIC PRESSURE DURING TAXI. REPAIR WIRE ON HYDRAULIC PRESSURE TRANSMITTER IAW MM 20-51-00; OPERATIONAL CHECK NORMAL IAW MM 20-00-00.SDR ARWA20061001Compressor · stalledLOG PAGE NR 124562. ABORTED TAKEOFF AT 105 KTS FOLLOWING NR 4 ENGINE COMPRESSOR STALL. INSPECTED NR 4 ENGINE COMPRESSOR SURGE BLEED VALVE AND TIGHTEN ALL SENCE LINES IAW MM 75-30-01/201; OPERATIONAL CHECK NORMAL ON ENGINE RUN IAW M/M 71-00/501.SDR ARWA20060602O-Ring · leakingPRIOR TO DESCENT, OBSERVED A LOSS OF HYDRAULIC QUANTITY TO THE STAND PIPE LEVEL FOLLOWED BY A LOSS OF PRESSURE. REMOVED AND REPLACED DAMAGE O-RING ON NR 2 ENGINE HYDRAULIC PUMP PRESSURE LINE FITTING IN ACCORDANCE WITH M/M 20-12-0 PAGE 211. OPERATIONAL CHECK SDR ARWA20060501Striker · unknownAFTER NORMAL GEAR RETRACTION, RED DOORS NOT LATCHED, LIGHT ILLUMINATED ON UP-LATCH CHECK; PERFORMED ABNORMAL CHECKLIST, LIGHT REMAINED ON. REMOVED AND REPLACED LT MAIN GEAR INBOUND DOOR LATCH STRIKER IN ACCORDANCE WITH M/M 32-31-4; ALSO REPLACED BOTH TARGET ASDR ARWA20060304Engine · leakingDURING CRUISE, NR 2 ENGINE LOSS OF ALL OIL QUANTITY AND PRESSURE; PRECAUTIONARY ENGINE SHUTDOWN AS PER CHECKLIST (TIME 0655). REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH ARROW AIR TASK CARD NR DC8-N-003. LEAK CHECKED, NO LEAKS NOTED; OPERATIONAL CHECKSDR ARWA20060302Proximity Switch · malfunctioned"GEAR NOT LATCHED" LIGHT ILLUMINATED AFTER GEAR UPLATCH CHECK; CONTINUED OPERATION AS PER ABNORMAL CHECKLIST. PERFORMED PROXIMITY SWITCHES TEST IN ACCORDANCE WITH M/M 32-60-0. REMOVED AND REPLACED CONTROL BOX PROXIMITY SWITCHES SYSTEM OPERATIONAL CHECK NORMASDR ARWA20060202Engine · vibrationSHUT-DOWN NR 3 ENGINE IN FLIGHT DUE TO VIBRATION. COMPLIED WITH ALL CHECKLIST. C/W RED BORDER NR 019421 NR 3 ENGINE P-679000 REPLACEMENT. COMPLY WITH RED BORDER NR 019421; REMOVED AND REPLACED NR 3 ENGINE IN ACCORDANCE WITH MAINTENANCE MANUAL 71-00-00. OPESDR ARWA20060218Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPARTMENT INTERIOR STA 1620-STA 1640 BETWEEN L-32L & L-33L SKIN WITH CORROSION; N/R 1022- AFT ACCESSORY COMPARTMENT INTERIOR STA 1620 BETWEEN L-30L & L-31L SKIN WITH CORROSION. REPAIR INNERSDR ARWA20060207Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1690 THRU STA 1720, L-31L THRU L-31R SKIN PANEL WITH CORROSION AT SEVERAL PLACES. REPAIRED FUSELAGE TAIL SECTION PLATING BETWEEN FS 1690 TO FS 1720 AND L-28R TO L-34 IN ACCORDANCE WITH DSDR ARWA20060217Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; I/B AILERON BETWEEN XA 565 AND SA 542 LOWER SKIN WITH CORROSION. REMOVED SKIN AND BONDED DOUBLER AND REPLACED BY SOLID SKIN BETWEEN XA 542 AND XW 563 IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-07/05. ISSSDR ARWA20060216Skin · corrodedDURING "C" CHECK INSPECTION, RT ELEVATOR XE 276 THRU XE 280 LOWER SURFACE WITH CORROSION. REMOVED RT ELEVATOR SKIN UPPER SURFACE XAE 0 TO XE 103 AND XE 273 TO XH 285 AND REPLACED WITH SOLID SKIN IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-05-05. ISSUED FAA FSDR ARWA20060215Skin · delaminatedDURING "C" CHECK INSPECTION, RT ELEVATOR XE 28.843 LOWER SURFACE WITH DELAMINATION. REMOVED RT ELEVATOR SKIN UPPER SURFACE BETWEEN XAE 0 TO SE 103 AND XE 273 TO XE 285 AND REPLACED WITH SOLID SKIN IN ACCORDANCE WITH DRAWING AIPSAC-N784AL-05/05. ISSUED FAA FOSDR ARWA20060214Finger Doubler · corrodedDURING "C" CHECK INSPECTION, MAIN CARGO COMPARTMENT STA.920, STA.940, STA.960, XCW 0 - XCW 23 CENTER WING SECCTION RT FINGER DOUBLER WITH CORROSION. REPAIRED FUSELAGE CENTER SECTION PRESSURE PANEL BETWEEN STA 920 AND FS 940 IN ACCORDANCE WITH DRAWING AIPSAC-SDR ARWA20060213Skin · corrodedDURING "C" CHECK INSPECTION, FUSELAGE EXTERIOR BETWEEN STA 1690 & STA 1734 AND L-26L THRU L-28L SKIN WITH CORROSION. REPAIRED FUSELAGE TAIL SECTION PLATING BETWEEN FS 1696 TO FS 1766 AND L-24L TO L-28L IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-03/05, SHEETSSDR ARWA20060212Skin · damagedDURING "C" CHECK INSPECTION, LT O/B AILERON BETWEEN XA 678 AND XA 685 LOWER SKIN RIVETS SHEARED. REMOVED LT O/B AILERON PLATING BETWEEN XA 662 & XA 724 AND REPLACED WITH SOLID SKIN IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-09/05, ISSUED FAA FORM 8110-3 APPRSDR ARWA20060210Structure · crackedDURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON FOOT STOOL I/B SIDE WITH 1 - 3/4" CRACK. REMOVED AND REPLACED NR 3 PYLON FOOT STOOL FITTING IN ACCORDANCE WITH DC8 S/B AS7-99 REVISION 1 DATED 09/03/93 AND DC8 S/B AS7-87, REVISION NR 2, DATED 01SDR ARWA20060209Skin · corrodedDURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPT INTERIOR STA 1620 BETWEEN L-30L AND L-31L SKIN WITH CORROSION. REPAIRED INNER DOUBLER BETWEEN FS 1620 AND FS 1680 AND L-26L AND L31L IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-06/05, ISSDR ARWA20060206Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STATION 1490 THROUGH STATION 1690L, L-31L THRU L31R SKIN PANEL WITH CORROSION AT SEVERAL PLACES. REMOVED AND REPLACED SKIN FROM FUSELAGE STA 1490 TO FS STA 1690 IN ACCORDANCE WITH AIPSAR EA SDR ARWA20050908Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; RT INBOUND AILERON BETWEEN XA 565 AND XA542 LOWER SKIN WITH CORROSION.SDR ARWA20050906Skin · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STA 1690 THROUGH STA 1734, L-29L, SKIN WITH CORROSION.SDR ARWA20050907Structure · crackedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 2 PYLON FOOT STOOL INBOUND SIDE WITH CRACK, APPROXIMATELY 5/8".SDR ARWA20050905Structure · crackedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 3 PYLON FOOT STOOL INBOUND SIDE WITH 1.750 INCH CRACK.SDR ARWA20050904Skin · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPT INTERIOR STA 1620 THROUGH STA 1640, BETWEEN L-32L AND L-33L, SKIN WITH CORROSION.SDR ARWA20050903Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1690 THROUGH STA 1720, L-31L THROUGH L-31R, SKIN PANEL WITH CORROSION AT SEVERAL PLACES.SDR ARWA20050902Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1490 THROUGH STA 1690, L-31L THROUGH L-31R, SKIN PANEL WITH CORROSION AT SEVERAL PLACES.SDR ARWA20050505Connector · dirtyDURING MAINTENANCE INSPECTION, NR 2 FIRE WARNING DOES NOT TEST; NO LIGHT; NO BELL. CLEANED NR 2 FIRE CONNECTOR WARNING; OPERATIONAL CHECK TEST NORMAL IN ACCORDANCE WITH M/M 26-10-0.SDR ARWA20050108Landing Gear · lack of lubeGEAR NOT LATCHED LIGHT ILLUMINATED. REMAINED ILLUMINATED AFTER COMPLETING GEAR NOT LATCHED LIGHT ILLUMINATED CHECKLIST. CHECK LANDING GEAR MECHANISM, LUBRICATED SAME, PERFORM GEAR SWING IN ACCORDANCE WITH MM 32-30-0. ALL LIGHTS OPERATED OK IN ACCORDANCE WITSDR ARWA20050106Engine · malfunctionedNR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED; OIL PRESS GAUGE INDICATED 25 PSI, FOLLOWED BY A LOSS OF OIL QUANTITY, WENT TO ZERO. PERFORMED OIL PRESSURE LIGHT ILLUMINATED CHECKLIST; THEN, PERFORMED IN-FLIGHT ENGINE SHUTDOWN ABNORMAL CHECKLIST. ENGINE SHUTDOWN SDR ARWA20050102Warning Light · illuminatedAFTER GEAR RETRACTION, GEAR NOT LATCHED LIGHT REMAINTED ILLUMINATED, PERFORMED ABNORMAL CHECKLIST. CHECKED ALL WIRING FOR GEAR LATCH LIGHT. JACKED A/C PERFORMED GEAR SWING SEVERAL TIMES. CHECK ALL THREE GEARS FOR CONDITION AND FOUND NORMAL. UNABLE TO DUPLISDR ARWA20041008Indicator · inoperativeLOST WEATHER RADAR IN ROUTE TO GEG. REMOVED AND REPLACED RADAR INDICATOR AND RADAR R/T, OPERATIONS TESTED NORMAL IN ACCORDANCE WITH M/M 34-41-1.SDR ARWA20040806Link Assy · failedAFTER TAKEOFF, HAD A VIBRATION BELOW COCKPIT AREA RECYCLED LANDING; GEAR NO HELP; RETURNED TO DEPARTURE (KMIA. REMOVED AND REPLACED RT NOSE GEAR DOOR LINK ASSEMBLY IAW MM 32-22-2. OPERATIONAL CHECK NORMAL.SDR ARWA20040501Indicator · malfunctionedSTANDBY ALTITUDE INDICATOR FAILED IN FLIGHT. REMOVED STANDBY INDICATOR & REPLACED WITH SERVICE STANDBY ATT. INDICATOR. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH DACO DC-8 MM 24-3-3.SDR ARWA20040502Wire · damagedNR 1 OIL TEMPERATURE ERRATIC AND UNREALIABLE IN-FLIGHT. REPAIRED WIRE AT PIN U NR 1 ENGINE PYLON MAIN DISCONNECT PLUG IN ACCORDANCE WITH DACO DC-8 MM 20-50-1. RAN ENGINE FOR 20 MINUTES. OPERATIONAL CHECK GOOD IAW DACO DC-8 MM 71-00-00SDR ARWA20031105Compressor · stalledON FLIGHT 410, THE NR 4 ENGINE COMPRESSOR STALLED, FOLLOWED BY LOSS OF POWER. ACCOMPLISHED IN FLIGHT ENGINE SHUTDOWN AS PER FOM; ENGINE SHUTDOWN AT 14:35, THE WINDMILLING OIL PRESSURE WAS ZERO.SDR ARWA20031101Brake Assy · damagedAIRCRAFT DOES NOT TAXI UNDER IT'S OWN POWER. FOUND NR 6 BRAKE ASSEMBLY DAMAGED. REMOVED AND REPLACED BRAKE ASSEMBLY IAW DC8 MM 32-42-1 AND MAIN WHEEL ASSEMBLY IAW MM 32-40-1. OPERATIONAL CHECK NORMAL.SDR ARWA20031001Link · brokenON APPROACH, WHEN SELECTING FLAPS 23 DEGREES AIRCRAFT ROLLED TO THE LEFT WITH SPLIT FLAP INDICATION, ON POST FLIGHT FOUND RT INBOARD FLAP BRACKET BROKEN. RECORD FOR 27-268. REMOVED AND REPLACED RT INBOARD FLAP IAW MM 27-51-4. OPERATIONAL CHECK NORMAL IAW 27SDR ARWA20030705Spring · brokenLOG PAGE 102010. AFTER TAKEOFF, DOORS NOT LATCHED LIGHT ILLUMINATED. FOUND BROKEN SPRING AT RT MAIN LANDING GEAR DOOR CONTROL VALVE MECHANISM. REPLACED SPRING IAW MM 32-32-7, PERFORMED GEAR SWING IAW MM 32-30-0; FOUND NORMAL SYSTEM.SDR ARWA20030512Skin · corrodedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR SURFACE WITH CORROSION, STATION 510, L-35R. REPAIRED FUSELAGE LOWER SKIN AT FUSELAGE STA 510 AND L-35R IAW AVITAS ENGINEERING REPAIR ORDER AROW-031RO-5, PAGE 1 & 2, DATED 05/01/03 AND REPAIRSDR ARWA20030511Skin · corrodedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT FUSELAGE INNER SKIN WITH CORROSION BETWEEN STATION 1660 AND STATION 1680, BETWEEN L-24R AND L-25R. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, REMOVED DAMAGED AREA SDR ARWA20030510Skin · corrodedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR LOWER SURFACE RIVET PLUNGED, STATION 540, BY L-36. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, TRIMMED SDR ARWA20030509Doubler · corrodedDURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT STATION 1620, BETWEEN L-26R AND L-31R INNER SKIN WITH SEVERAL SPOTS OF CORROSION. REPAIRED FUSELAGE INNER DOUBLER AT FS 1620, BETWEEN L-25R AND L-31R IAW MFG ENGINEERING REPAIR OSDR ARWA20030508Fitting · crackedN/R 421. DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR WHEEL WELL STATION 879, L-24R FITTING WITH CORROSION AND 3 INCH CRACK. REMOVED AND REPLACED FITTING OF R/H MAIN LANDING GEAR WHEEL WELL STA 879, L-24R IAW SRM 51-1-20D AND SR
Back to N784AL, cancelled Feb 16, 2017