N718BA
Service difficulty reports · 77
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 = 'N718BA' AND registry_match = 'registration' 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 = 'N718BA' AND registry_match = 'registration' 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 UIEA2014101000480Keelbeam · corrodedCORROSION THE UPPER CHORD OF THE KEEL BOX BETWEEN STATION 1286 TO 1289.5, WL 116, LBL 9 LT WING GEAR WHEEL. REPAIRED IAW EI NO T2014A53B 3027 REV 2. CONDITION CHECKED NORMAL.SDR UIEA2014101000481Cargo Track · damagedFOUND THE WEAR DAMAGED ON THE LT & RT MAIN DECK CARGO RAIL AT STATION 600 TO 2053 BL 98.2. ACCOMPLISHED EI NO T2014A25B 3284 REV 0. JOB COMPLETED & CONDITION CHECKED NORMAL.SDR UIEA2014101000482Shear Tie · corrodedCORROSION FRAME SHEAR AFT CARGO COMPARTMENT, STATION 1860 STRINGER 47L - 48L. REPAIRED DAMAGE AREA IAW EI NO T2014A53B 2784 REV 2. JOB COMPLETED & CONDITION CHECKED NORMAL.SDR UIEA2014101000483Floor Panel · crackedFOUND COCKPIT PILOT SIDE FLOOR PANEL CRACK STATION 318 LBL 30. ACCOMPLISHED REPAIR IAW T2014A53B-3153 REV 2. JOB COMPLETED & CONDITION CHECKED NORMAL.SDR UIEA2014101000485Keelbeam · corrodedCORROSION THE UPPER CHORD OF THE KEEL BOX STATION 1350, BL 0, WL 116.06 RT & LT WING GEAR. REPAIR DAMAGE AREA IAW EI NO IAW T2014A53B-2731 REV 9. JOB COMPLETED & CONDITION CHECKED NORMAL.SDR UIEA2014101000487Battery · dischargedFOUND THE L1 DOOR EMER LIGHT POWER SUPPLY X317 INOPERATIVE. R & R UPPER DECK DOOR SLIDE LIGHT BATTERY & LIGHT TESTED SATISFACTORY IAW AMM 33-51-06 REV 81.SDR UIEA2014051400184Accelerometer · faultyNUMBER 3 ENG HIGH VIB INDICATION IN CRUISE LEVEL 4. R & R NR 3 ENG ACCELEROMETER IAW 77-31-01-404-007 & N00-AVM, SYS CHECKED NORMAL. R & R NR 3 ENG SPINNER IAW AMM 72-31-01, NR 3 ENG VIBRATION SURVEY SATISFACTORY.SDR UIEA2013031800138Frame · damagedFRAME WAS FOUND TO HAVE BENT AND CRACKED AREA IN ITS LOWER FLANGE NEAR BS 260 ON THE LEFT HAND OTBD SIDE OF THE NOSE WHEEL WELL OPENING. THE FORWARD DAMAGE WAS APPROX 1.5" LONG. THE CHORD IS A 7075-T62 EXTRUSION IAW DWG 65B07942. THE DAMAGED FRAME WAS REPAIRSDR UIEA2013031300128Actuator · failedAFTER TAKEOFF, DURING GEAR RETRACTION A LOUD BANG WAS HEARD AND A HEAVY VIBRATION WAS FELT COMING FROM THE NOSE GEAR AREA, FOLLOWED BY A TOTAL LOSS OF HYD SYS NR 1. ON INVESTIGATION, NOSE GEAR DOOR ACTUATOR WAS FOUND TO BE FAILED CAUSING TOTAL FLUID LOSS. NOSDR UIEA2013020700074Warning Message · false activationSTATUS MESSAGE LOWER EICAS SCREEN: SWG TL SW S2497- SWING TAIL LATCH/ LOCK INDICATION SYS - CLOSED/ LATCHED LIMIT SWITCHES, EICAS INDICATES NORMAL CMC INDICATES NO FAULTS.SDR UIEA2013020400066Skate Angle · crackedCRACK ON THE SKATE ANGLE OF NR 3 PYLON INBD FAIRING AT NAC STA 457. REPAIRED IAW EI NR T2013A54B-290, REV 00 AND REV 01.SDR UIEA2013020400067Structure · damagedCRACK ON THE UPPER BIFURCATION WALL OF NR 1 RT THRUST REVERSER. REPAIRED IAW EI NR T2013A78B-309, REV 00 AND REV 01.)SDR UIEA2012043000170Light · inoperativeL1 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REMOVED AND ATTEMPTED TO CHARGE THE L1 DOOR SLIDE EMERGENCY LIGHT ASSY POWER PACK. INSTALLED SAME LIGHT ASSY IAW AMM 33-51-06 BUT OPS CHECK FAILED.SDR UIEA2012032300102Autothrottle Sys · slowEXTREMELY SLOW AUTO THROTTLE RESPONSE. MODERATE TO SEVERE TURBULANCE ENCOUNTERED. ADVANCING THROTTLE RESULTED IN ACFT OVERSPEED, THEN 20 KTS LOW. AUTO THROTTLE TURNED OFF. SEVERE TURBULENCE ENCOUNTERED FOR 10 MINUTES. PERFORMED OPS CHECK OF LT FMC FOR PRESSDR UIEA2012030200074Switch · out of sequenceEICAS MSG GEAR DOOR. FOUND ALTERNATE EXTENTION SYS OUT OF SEQUENCE, RESET ALTERNATE GEAR EXTENSION SWITCH IAW MM 32-35-00 AND DID AN OPS CHECK IAW MM 32-35-00.SDR UIEA2011122100725Fairing · damagedDURING WALKAROUND, DAMAGE WAS FOUND TO THE RT AFT WING TO BODY FAIRING AT BS 1560, APPROX STRINGER 38R.; THE AIRPLANE HAS 8,082 TFC AND 60,711 TFH AT THE TIME OF THE PART 1 REPAIR. THE DAMAGE CONSISTS OF A HOLE IN THE WING TO BODY FAIRING HONEYCOMB STRUCTURE MSDR UIEA2011071600365Battery Pack · dischargedFOUND MAIN DECK EMERGENCY LIGHTS INOPERATIVE. IAW AMM 33-51-04-902-001-001, REV 71, REPLACED EMERGENCY LIGHT BATTERY AND PERFORMED OPS TEST. RESULT WAS SATISFACTORY.SDR UIEA2011071100362Skin · damagedBENT DAMAGE ON THE AFT CARGO DOOR FWD LOWER EDGE SKIN. (REPAIR - IAW EI NR T2011A52B - 1503 REV 00. AND REV 01)SDR UIEA2011070800360Keelbeam · corrodedLEVEL II CORROSION ON KEELBEAM NEAR BS 1307,WL 116, LBL 9. CORROSION WAS BLENDED. BLENDED AREA WAS SHOT PEENED, ALODINED, PRIMED AND TOP COATED USING WHITE ENAMEL. A LAYER OF CORROSION COMPOND WAS APPLIED TO THE REWORKED AREA. AFTER REWORK THE DAMAGE IS CSDR UIEA2011070700366Frame · corrodedCORROSION ON FWD LOWER CHORD (PN 65B15207-15) OF BULKHEAD AT STA 1348, RBL 49.5. (REPAIR IAW EI NR T2011A53B-1529, REV 00 AND REV 01 AND REV 02.)SDR UIEA2011070700364Stiffener · corrodedCORROSION ON STIFFENER. PN 65B10497-601 OF KEEP TORQUE BOX AT STA 1416 RBL 5. RT W/W. (REPAIRED IAW EI NR T2011A53B-1527 REV 00 AND REV 01, REV 02.SDR UIEA2011070700363Structure · corrodedCORROSION ON UPPER CHORD PN 65B10994-10 OF KEEL TORQUE BOX AT STA 1276, RBL 9, RT WING W/W. (REPAIR IAW EI NO T2011A53B-1522 REV 00. AND REV 01, REV 02.)SDR UIEA2010071200107Skin · crackedAN INSP IN THE UPPER FWD CORNER SKIN OF THE AFT CARGO DOOR CUTOUT REVEALED A CRACK (REPAIRED IAW SB 747-53A2448, REV 1 AND SRM 53-60-01, FIG 201, REPAIR 3 WITH A REVISED FASTENER PATTERN AND (2) FASTENERS OVERSIZED BEYOND THE SRM LIMITATIONS, SEE FIGURE 1. THSDR UIEA2010070900096Skin · corrodedCORROSION WAS FOUND ON THE RT INBD MID FLAP UPPER SKIN AT WBL 315 AND 388. LEVEL 1 CORROSION. (THE CORROSION WAS BLENDED OUT TO A MINIMUM THICKNESS OF 0.070 INCH, NDI INSPECTED, THE SURFACE FINISH WAS RESTORED AND A BONDED FILLER AND REPAIR DOUBLER WAS INSTALLSDR UIEA2010070800112Skin · corrodedDURING THE D-03 CHECK, CORROSION FOUND ON RT WING T/E, LOWER SKIN 112U4502-2 WHICH MATING WITH FIXED PANEL 112U4710-38 AT WBL 1144. LEVEL 1 CORROSION. (CORROSION WAS COMPLETELY REMOVED AND THE BLENDED SKIN AREA AND FASTENER HOLES ARE DET/HFEC INSPECTED TO CONSDR UIEA2010070700095Strut · gougedDURING THE LCF MODIFICATION IN TPE AND INSP IAW SB 747-54A2218 (AD 2005-19-09), A GOUGE WAS FOUND IN THE NR 4 STRUT LT SIDE & NBSP; LINK & NBSP; DO NOT SCHEDULE; THIS EO DOCUMENTS AN INTERIM REPAIR ACCOMPLISHED AT TPE DURING THE SEPTEMBER 2008 LCF MODIFICATIONSDR UIEA2010063000055Skin Panel · damagedDURING THE LCF MODIFICATION IN TPE, THE SKIN PANEL FROM BS 340 TO 520, S-6L TO -14L WAS REPLACED IAW EGAT EI B2008A53M-048 AND NRC U09082. DURING THE PANEL REPLACEMENT, SHORT EDGE MARGINS WERE FOUND IN THE STRAPS AND DOUBLERS IN THE SKIN PANEL. (THE SEM WAS R
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