N919FD
Service difficulty reports · 203
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 = 'N919FD' 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 = 'N919FD' 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 FDEA201410173251Bracket · looseRIGHT WING FAIRING 672HB BRACKET INBD SECURING BRACKET FOUND LOOSE FLAP. REPAIRED IAW EA F-5720-T0312233.SDR FDEA201410173285Skin · puncturedRIGHT WING INBD FLAP UPPER SURFACE FOUND TO HAVE SMALL PUNCTURE HOLE. REPAIRED IAW SRM 51-70-17 TRACKING EA F-5750-T0312308.SDR FDEA201410163226Skin · damagedLIGHTNING STRIKE DAMAGE TO CROWN SKIN BS 1335 STRINGER 1. REPAIRED IAW EA 5300-T0312097.SDR FDEA201410163225Wedge · damagedNUMBER 5 SLAT FOUND TO HAVE TE WEDGE DISBONDED ON OTBD LOWER SURFACE. REPAIRED IAW EA F-5750-T0311994.SDR FDEA201410163224Wedge · debondedNUMBER 1 SLAT TE WEDGE DISBONDED ON UPPER & LOWER SURFACES. REPAIRED IAW EA F-5750-T0311993.SDR FDEA201410163211Skin · damagedLEFT WING OTBD MAIN FLAP LE BULLNOSE DAMAGED. REPLACED IAW SRM 51-40-02 & DWG 113N3500.SDR FDEA201410163210Skin · damagedTHREE LIGHTNING STRIKES FWD OF E & E BAY DOOR. REPAIRED IAW SRM 53-00-01.SDR FDEA201410163208Skin · damagedLIGHTNING STRIKE FOUND AT BS 215 STRINGER 27L. REPAIRED IAW SRM 53-00-01.SDR FDEA201410163207Structure · corrodedSURFACE CORROSION ON FWD SHEAR DECK AFT OF 9G BARRIER. REMOVED IAW SRM 51-20-01. REPAIR CARRIED OUT IAW EA F-5300-T0311939A. REPAIR CLASSED AS MINOR.SDR FDEA201410163206Skin · damagedBS 215 LIGHTNING STRIKE BETWEEN STRINGER 25 - 26L. REPAIRED IAW EA F-5300-T0312150.SDR FDEA201410163205Skin · dentedSUSPECT DENT LOCATED APPROX BS 213 STRINGER 26 - 27L. ASSESSED & REPAIRED IAW EA F-5300-T0312150.SDR FDEA201410153162Arm · damagedRIGHT WING MLG REAR MOVEABLE FAIRING 671BB ACTUATING ARM FOUND DAMAGED. INVESTIGATE & RECTIFY IAW AMM SRM RT MLG MOVEABLE FAIRING 671BB ACTUATING ARM BLENDED & REPAIRED IAW F-5720-T0311986. REPAIR CLASSED AS MAJOR REPAIR, JPF STAGES SHOW DETAILS OF INITIAL BSDR FDEA201410042964Gate · corrodedNUMBER 2R DOOR LOWER GATE EDGE IS CORRODED. NR 2R DOOR LOWER GATE REPLACED IAW AMM 52-11-38-4SDR FDEA201410042963Gate · chafedNUMBER 4R DOOR LOWER GATE AFT EDGE HAS CHAFING DAMAGE. NR 4R DOOR LOWER GATE ASSEMBLY REPLACED IAW AMM 52-11-38-4.SDR FDEA201410022924Skin · wornRIGHT WING OTBD FLAP LE BULLNOSE PAINT WORN AT INBD END RT WING OTBD FLAP LE BULLNOSE WEAR ASSESSED OUT OF LIMITS 2 INCHES X 1.25 INCHES X 0.046 INCHES, BULLNOSE SECTION REPLACED IAW SRM 51-40-02 & DWG 113N3500.SDR FDEA201409292853Skin · damagedLIGHTNING STRIKE DAMAGE BS 1220 STRINGER 1 FASTENER. REPAIRED IAW SRM 53-00-01 REPAIR 6.SDR FDEA201409292852Skin · damagedLIGHTNING STRIKE TO FUSELAGE BS 1460 STRINGER 1R. REPAIR CARRIED OUT IAW SRM 53-00-01 REPAIR 6.SDR FDEA201409272829Gate · corrodedL1 DOOR LOWER GATE EDGE IS CORRODED. L1 DOOR LOWER GATE REPLACED IAW AMM 52-11-38-4SDR FDEA201409242759Skin · damagedL1 DOOR SNUBBER SPRING CANISTER ASSEMBLY FOUND TO BE FOULING ON FUSELAGE SKIN INBD OF SPRING CANISTER. SKIN PANEL REPLACED IAW SRM 51-40-02, 51-40-05 REF DWG 141N8315.SDR FDEA201401100078Charger · inoperativeDURING SERVICE CHECK, FOUND L1 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. CHECKED FOR 28VDC AT LAMP & FOUND NO POWER, CONFIRMED GOOD GROUND. R & R EMERGENCY LIGHTS POWER SUPPLY, & BATTERY CHARGER, IAW AMM 33-51-07-2. PERFORMED OPS CHECK IAW AMM 33-51-06-2-1 SDR FDEA201310112473Controller · failedPRESSURIZATION SYSTEM 2 WOULD NOT MAINTAIN CABIN ALTITUDE. CABIN ALTITUDE CONTINUOSLY ROSE, DESCENDED TO FL 100. FOUND NR 2 CABIN PRESSURE CONTROLLER AT FAULT. REPLACED CONTROLLER IAW AMM 21-31-02-4.SDR FDEA201304170795Cylinder · leakingAFTER BLOCK IN, ARRIVAL PERSONNEL OPENED DOOR WHILE SLIDE WAS ARMED FROM OUTSIDE. SLIDE BOTTLE BLED OUT AND GIRT BAR IS SLIGHTLY AJAR. REMOVED RED EMERGENCY POWER SPRING CYLINDER IAW MM 52-11-33-4. ACFT OK TO CONTINUE.SDR FDEA201208243151Valve · malfunctionedAFTER EXTENDING THE LANDING GEAR FOR LANDING. LANDING GEAR "DOORS" LIGHT DID NOT EXTEND. R & R DOWNLOCK VALVE PER AMM 32-32-07-4. MAIN GEAR DOWNLOCK, OPERATED DOOR SEQUENCE PERFORMED CHECK OF THE UPLOCK OPERATE SEQUENCE VALVE PER SUBTASK 32-32-09-864-014SDR FDEA201204271653Apu · smokePRIOR TO START CHECKLIST, ACRID SMOKE ENTERED COCKPIT. INTITALLY SMELLED SMOKE, THEN VISIBLE. APU RUNNING, BOTH LT & RT PACKS ON. TURNED OFF PACKS & OPENED WINDOWS TO VENT COCKPIT. SMOKE STOPPED AFTER PACKS TURNED OFF. PRIOR TO DECLARING SMOKE IN COCKPISDR FDEA201111245019Fuel Cell · corrodedCENTER TANK UPPER SKIN UPPER SURFACE FOUND CORRODED AT BS 920 , AT AREA JUST UNDER RT STUB BEAM CORROSION. REMOVED AND ASSESSED IAW SRM 57-10-01 MAX BLEND MATERIAL REMOVED 0.013 " MAX LIMIT 0.028" BLEND FOUND TO BE WITHIN LIMITS. DUE TO ACCUMALATIVE BLENDSSDR FDEA201111245016Crease Beam · corrodedRT CREASE BEAM CORRODED AROUND ANCHOR NUT HOLES APPROX BS 1020-1040. CORROSION FOUND TO BE OUT OF LIMITS. REPLACEMENT FABRICATED IAW DWG 144N5140 AND INSTALLED IAW SRM 51-40-02.SDR FDEA201111245015Crease Beam · corrodedLEFT CREASE BEAM INBD CHORD CORROSION FOUND AROUND ANCHOR NUT HOLES APPROX BS 1020-1040, CORROSION FOUND TO BE OUT OF LIMITS. REPLACEMENT CHORD FABRICATED IAW DWG 144N5140 AND INSTALLED IAW SRM 51-40-02.SDR FDEA201111235014Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING SKIN BENEATH STUB BEAM AT BS940, LBL65. REPAIR CARRIED OUT IAW EA F-5710-154331.SDR FDEA201111184967Skin · damagedLIGHTENING STRIKE ON FUSELAGE SKIN, BS 1240 S7-8R. REPAIR CARRIED OUT TO SKIN IAW EA F-5300-154337.SDR FDEA201111184966Skin Panel · damagedLIGHTNING STRIKE AT STA 1160-1180, ST7, REPAIR CARRIED OUT IAW EA F.5300-154337.SDR FDEA201111084818Skin · damagedFUSELAGE SKIN HAS A LIGHTNING STRIKE AT BS 1360 S7-8R. REPAIR CARRIED OUT IAW EA F-5300-154337.SDR FDEA201111084809Skin · damagedSKIN HAS A LIGHTENING STRIKE AT BS 1520 S8R. REPAIRED IAW EA F-5300-154337.SDR FDEA201111084805Beam · corrodedWING CENTER TANK, UPPER SURFACE BS 940 STUB BEAM CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-51. NEW STUB BEAM FABRICATED IAW DWG 144N1019 AND FITTED.SDR FDEA201111084807Skin · corrodedEXFOLIATION CORROSION FOUND ON UPPER WING SKIN BENEATH STUB BEAM AT RBL 65 REPAIR CARRIED OUT IAW EA F-5710-154331.SDR FDEA201111084802Fuel Cell · corrodedCENTER TANK UPPER SKIN SURFACE ATTACHED REPAIR PATCH AT BS 980-1000 RT STUB BEAM AREA FOUND DISBONDED. CORROSION REMOVED FROM AFFECTED AREA REPAIR CARRIED OUT IAW EA F-5710-154339.SDR FDEA201111084804Fuel Cell · corrodedCORROSION FOUND BENEATH STUB BEAM ON CENTER TANK SKIN AT BS 940 LT AND RT SIDE OF CABIN CORRODED AREAS REPAIRED IAW EA F-5710-154331.SDR FDEA201111084803Fuel Cell · corrodedCTR TANK UPPER SKIN UPPER SURFACE ATTACHED REPAIR PATCH AT BS 960-980 LT STUB BEAM AREA FOUND DISBONDED. CORRODED AREA BLENDED AND REPAIRED IAW EA F-5710-154339.SDR FDEA201111084810Bearing · corrodedL1 DOOR EMERGENCY POWER TRIGGER MECHANISM CABLE ACTUATION BELLCRANK SEIZED DOOR TRIGGER QUADRANT BEARINGS FOUND SEIZED RERIG OF DOOR CARRIED OUT POST BEARING CHANGE IAW 52-1136.SDR FDEA201111084808Skin · damagedLIGHTNING STRIKE AT STA 1460 ST 8-9R LIGHTNING STRIKE REPAIR CARRIED OUT IAW EA F-5360-154332.SDR FDEA201110284678Bearing · corrodedL1 DOOR EMERGENCY POWER TRIGGER MECHANISM CABLE ACTUATOR BELLCRANK SEIZED. TWO OFF BEARINGS IN CABLE ACTUATING BELLCRANK REPLACED.SDR FDEA201110184571Fuel Cell · corrodedEXFOLIATED CORROSION FOUND BENEATH STUB BEAM AT BS940 LT SIDE OF CABIN AT CENTER TANK SKIN. REWORK CARRIED OUT ON NON ROUTINE N00425 AND EA F-5710-154331.SDR FDEA201103080905Skin · delaminatedDELAMINATION FOUND ON SLAT1 OTBD UPR T/E FROM OTBD END TO 250MM AND 40MM FROM T/E DIM 250MMX40MM, 15SQIN. REPAIRED IAW SRM 57-70-10CH REPAIR #4, 57-43-02 FIG 1 AND FIG 201REPAIR DOUBLER INSTALLED,SDR FDEA201007082415Transmitter · malfunctionedREJECTED TAKEOFF AT 100KTS. AT 80KT POWER WAS SET TO STANDARD AT APPROX 1.57 EPR. AFTER 80 KTS NR 1 ENG PWR DECREASED ABOUT 10 PERCENT. ADVANCED NR1 THRUST LEVER AND NR1 EPR WOULD NOT RECOVERED. CHECKED EJECTOR FILTER AND FOUND CLEAN. PURGED EPR LINE AND R SDR FDEA201004221356Skin · damagedC-2 DOOR LOWER AFT CORNER EXTERNAL SKIN HAS TRIM OUT FGREATER THAN .001". FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071" DIMENSION 6 3/4" X 6 1/4" IAW SRM 52-30-1 FIGURE 201. TREATED AND PRIMED PARTS IAW SRM 51-20-1. INSTALLED REPAIR DOUBLER AT C-2 DOOR LOWER SDR FDEA201004221354Skin · damagedC-1 DOOR LOWER AFT CORNER EXTERNAL SKIN HAS ROUTE OUT GREATER THAN .001". CUT OUT DAMAGE DIMS 1 1/4" X 1/4" IAW SRM 52-30-1, FABRICATED REPAIR DOUBLER USING 2024T-3 .071 DIMS 5 7/8" X 5 3/4" IAW SRM 52-30-1 AND INSTALLED REPAIR DOUBLER IAW SRM 52-30-1.SDR FDEA201004221355Skin · damagedC-2 DOOR LOWER FWD CORNER EXTERNAL SKIN HAS TRIM OUT GREATER THAN .001". FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071" DIMENSION 6.7500" X 6.5" IAW SRM 52-30-1, FIG 201. TREATED AND PRIMED PARTS IAW SRM 51-20-1. INSTALLED REPAIR DOUBLER AT C-2 DOOR LOWER SDR FDEA200909193333Switch · out of positionAFTER TAKEOFF AND PASSING 10,000 FT, AIRSPEED ZIPPER DID NOT INCREASE TO EXPECTED CLIMB AIRSPEED, MAX AIRSPEED 268 KTS AT FL 360, ZIPPER RESTRICTED AIRSPEED TO 238 KIAS. DURING DESCENT, PASSING FL300 ZIPPER INCREASED TO 268. DURING APPROACH ZIPPER INDICATIONSDR 08FDEA04714Skin · chafedRT WING O/B MAIN FLAP O/B L/E CORNER HAS 4 INCH CHAFF MARK (FROM LOWER WING PANEL). DEFECT REPAIRED IAW EA F-5750-120571. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA03886Bulkhead · crackedNR 1 STRUT MID BULKHEAD LOWER FLANGES RT FWD FITTING BOLT HOLE CRACKED. REF CARD 5450-7-5005 P1 CARD 15 OF 33. NR 1 NACELLE STRUT MID-BULKHEAD LOWER FLANGE RT FWD FITTING BOLT HOLE REPAIRED IAW FEDEX EO F-5450-7-5005 PT 5. REPAIR IS CLASSIFIED AS MAJOR PER SDR 08FDEA03655Skin · corrodedRT WING TOP SURFACE REAR SPAR AREA APPROX WS 230-345, 3 SPOTS OF CORROSION ON TOP OF WING. REPAIR CARRIED OUT BY BLENDING OUT IAW B757-200 SRM 57-20-01 TABLE 1 AND EA F- 5730-124309. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.
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