N996FD
Service difficulty reports · 117
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 = 'N996FD' 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 = 'N996FD' 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 FDEA202609131331Ballscrew · failedFOUND LT WING FLAP INBD TRANSMISSION WITH INDICATOR TRIPPED & JACKSCREW DAMAGED. AMM: 27-51-11-4 AMM: 27-51-06-4 REMOVED INBD T/E FLAP XMISSION & INBD TE BALLSCREW IAW AMM. DIMENSION X NOTED AS 19.75 IN. FSEU-1 READINGS: LT FLAP 340.03 DEG, RT FLAP 340SDR FDEA202609111324Transmission · faultedWHEN FLAPS 20 SELECTED ON ARRIVAL TE FLAPS DISAGREE EICAS ALERT. TE FLAPS STOPPED AT APPROXIMATELY 18 DEGREES. DECLARED EMERGENCY, ACCOMPLISHED QRH PROCEDURE, LANDED FLAPS 20. EMERGENCY DECLARED. REPLACED #4 FLAP TRANSMISSION DUE TO OVERLOAD & DRAINED ANSDR FDEA202606230791Girt Bar · out of adjustRT ENTRY DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL : 52-11-01-A. R1 DOOR OR SLIDE INOP. ADJUSTED R1 DOOR GIRT BAR REF AMM 25-66-10-2. OPS CHECKED GOOD.SDR FDEA202606100695Door · fodCREW REPORTED R1 DOOR WILL NOT ARM AMM 52-11-25-5 REMOVED DEBRIS FROM AREA AND PERFORMED SATISFACTORY ARM AMD DISARM OF R1 DOOR. AMM 52-11-25-5 REMOVED DEBRIS FROM AREA AND PERFORMED SATISFACTORY ARM AMD DISARM OF R1 DOOR.SDR FDEA202505200770Battery Pack · failedR/H EMGERGENCY EXIT SIGN AND EXTERIOR LT INOP. REPLACED R/H EMGERGENCY EXIT SIGN AND EXTERIOR LT BATTERY PACK ASSY (RADIANT POWER CORP). OK FOR SERVICE.SDR FDEA202503050331Slide · partial deployL 1 DOOR SLIDE PARTIAL DEPLOYMENT DUE POSIBLE FOD IN GIRT BAR. ( GRAY MATS). REMOVED AND REPLACED L1 DOOR SLIDE. AMM: 25-66-01-4.SDR FDEA202407181030Iru · failedREJECTED TAKEOFF. SIMULTANEOUS L & C IRS FAULT EICAS AND ASSOCIATED ATT & HDG FAILURES. REFERENCE WRI 05-50-0566: ACCOMPLISHED WATER ACCUMULATION INSPECTION AND REMOVAL REF B757 MM 05-51-99-6. GVI FOUND NO WATER EVIDENCE ON ANY AVIONICS RACK DRIP PANS OR BSDR FDEA202404030441Window · arcedAT CRUISE FL360, R FWD WINDOW BEGAN ARCING FOR 20-30 SECONDS FOLLOWED BY THE OUTER PAIN SHATTERING. THE INNER PAIN APPEARS INTACT WITH NO LEAK OR LOSS OF PRESSURIZATION. ACCOMPLISHED ALL QRH PROCEDURES. CONTINUED AND LANDED DESTINATION WITH NO FURTHER ISDR FDEA202307251290Floorboard · delaminatedZONE 220 FLOORBOARD 221 MBF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221 MBF ON VT MAE TRAVELER # T23/1691348 IAW DWG SRZ -25-005 REVISION R MAJOR REPAIR.SDR FDEA202307251289Floorboard · damagedZONE 220 FLOORBOARD 221BF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221 BF ON VT MAE TRAVELET # T23/1691347 IAW DWG SRZ -25-005 REVISION R MAJOR REPAIRSDR FDEA202307211266Flap · damagedL/H WING O/B AFT FLAP LOWER SKIN APPROX. MID POINT HAS A REPAIR THAT IS NOT ON THE AGING MAJOR REPAIR LIST. VISUALLY INSPECTED REPAIR IAW ATTACHMENT "B" OF EO F-5100-7-5001. REPAIR APPEARS TO BE IN COMPLIANCE IAW SRM 57-53-01-2R REP # 1. CATEGORY "A" REPAISDR FDEA202307211265Web · damagedWEB REPAIR ON MAIN DECK AT STA1720 BL 0 TO LBL 47.5 IS NOT ON AGING MAJOR REPAIR LIST. VISUALLY INSPECTED REPAIR IAW ATTACHMENT "B" OF EO F-5100-7-5001. REPAIR APPEARS TO BE IN COMPLIANCE IAW SRM 53-60-51-2R REP 2. CATEGORY "A" REPAIR. CLASSIFIED AS A MAJOR SDR FDEA202307191242Seat Track · corrodedMAIN CABIN BETWEEN STA 1160 & 1200, RBL 45, SEAT TRACK FLANGE HAS CORROSION. REMOVED AND REPLACED SEAT TRACK FROM STA 1180-1230 RBL 45 PER SRM 53-00-52-2R REPAIR 3, FIGURE 101 AND SRM 51-40-02, MAJOR REPAIR.SDR FDEA202307131214Seat Track · corrodedCORRODED SEAT TRACK AT STA. 345.0 RBL 24. CORROSION ON SEAT TRACK WAS EVALUATED AND FOUND OUT LIMITS IAW B 757 SRM 53-00-52- 1A. FABRICATED NEW SECTION SEAT TRACK, LOCATED , DRILLED AND INSTALLED IAW B757 SRM 53-00-52-2R, FIG. 101, REPAIR 1, MAJOR REPAIR.SDR FDEA202212092895Slide · dislodgedAFTER L CREW ENTRANCE DOOR WAS OPENED, WITH NO SLIDE DEPLOYMENT, GROUND CREW OPENED THE ALREADY CRACKED, DISARMED DOOR AND DURING THE OPENING PROCESS THE SLIDE FELL OUT OF THE BOTTOM OF THE DOOR. AT THAT TIME THE SLIDE DID NOT INFLATE BUT DISCHARGED ITS GSDR FDEA202207151732Collar · crackedFOUND L1 DOOR HOLD-OPEN LOCK BROKEN. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK REF AMM 52-11-08-4. OK FOR SERVICE.SDR FDEA202203110494None · noneTE FLAP DISAGREE WHEN FLAPS 1 SELECTED. DID NOT CLEAR WITH QRH. PROCEEDED TO TE FLAP ASYM QRH AND LANDED WITH FLAPS SHOWING BETWEEN 0 AND 1. T/S AND FOUND THE LEFT INBOARD FLAP, INBOARD FLAP TRANSMISSION INDICATOR POPPED. RESET THE INDICATOR AND CHESDR FDEA202111272941Flap System · faultedTE FLAP DISSAGREE EICAS MSG WHEN FLAP HANDLE SELECTED AT 1. RAN CHECKLIST AND LANDED FLAPS 20 WITH NO FURTHER ISSUES. PERFORMED FSEU BITE PROCEDURE. NO FSEU HAD ANY CURRENT FAULTS, FSEU 1 HAD FAULT 224 "LEVER XMT" ON FLIGHT 0, FSEU 3 HAD FAULT 305 FLAP DSDR FDEA202108292155Skin · debonded#3 SLAT DISBOND INDICATION FOUND: T/E WEDGE LOWER SKIN 1.5" IN DIAMETER, 30" FROM O/B, 2" FROM TOP T/E REPLACED #3 SLAT PER B757 AMM 27-81-02-4SDR FDEA202108272119Attach Bracket · crackedEXTERIOR FUSELAGE NOSE RADOME HOLD OPEN ROD STOWAGE PIN ATTACH BRACKET IS DEFORMED ON THE LEFT FWD BULKHEADS WALL (ZONE 111) REMOVED DAMAGED BRACKET , INSTALLED SERVICEABLE BRACKET IAW DWG 141N7835 AND B757 SRM 51-40- 02-0GSDR FDEA202108262106Floorbeam · crackedMAIN FLOOR BEAM AT STA 580 LBL 45.5 IS CRACKED. REPAIRED FLOOR BEAM AT STA 580 LBL 45.5 IAW FEDEX E.A. F-5310-T0363608 AND FEDEX STANDARD REWORK DRAWING SR57-53-004.SDR FDEA202108252096Bracket · crackedWIRE CONDUIT BRACKET CRACKED BETWEEN FASTENER HOLES UNDER ACCESS PANEL 435AL REMOVED AND REPLACED BRACKET PER DWG 313N3053 REV ESDR FDEA202103040559Pump · leakingL HYD SYS PRESSURE LOSS OF LEFT HYD. QUANTITY "0". QRH REFERENCED. PTU FUNCTIONED PROPERLY. DECLARED EMERGENCY. REQUESTED TOW FROM MAINTENANCE. IND REMOVED AND REPLACED LEFT ENGINE DRIVEN HYDRUALIC PUMP CASE DRAIN MODULE IAW AMM 29-11-17-4. OPS CHECK LEAK SDR FDEA202009092156Holder · damagedMDIS 996, 33-50, 7681, 09SEP20, MEM, FACT, U. ON PREFLIGHT, DISCOVERED EMERGENCY LIGHTS FOR L1 DOOR, BOTH INTERIOR AND EXTERIOR, INOPERABLE. R/I 09SEP20 06:37 MEM U. REASON CODE: FAILED OPS CK & REPLACED WITH SERVICEABLE UNIT, OFF MPN: 2013-1A POS: 1 SRL: SDR FDEA202004230775Hydraulic Line · not reportedL HYD ELEC PUMP AND L HYD QTY EIAS AT CRUISE. FOLLOWED BY L HYD SYS PRESS. QRH COMPLETED EMERGENCY DECLARED. PTU OPERATED NORMALLY TO MAINTAIN L SYS PRESSURE ON STATUS PAGE. INSTALSDR FDEA2019123183322Light · false activationR1 ENTRY DOOR SLIDE LIGHT REMAINS ILLUMINATED WHEN SLIDE ARMING LEVER MOVED TO DISARM. CHECKED SWITCH SENSOR GAP IAW AMM 25-66-11-2 FIG 201 CHECKED GOOD. OPERATED ARMING LEVER SEVERAL TIMES IAW AMM 25-66-11-2. LIGHT INDICATION AND OPERATION CHECKED NORMAL.SDR FDEA2019120103157Transmitter · failedRIGHT ENG WOULD NOT RELIGHT AFTER INTENTIONAL SHUTDOWN FOR TEST FLIGHT PROFILE. ENGINE VALVE DISCREET LIGHT REMAINED ILLUMINATED WHEN RIGHT FIRE HANDLE WAS PULLED AND RESET. RIGHT ENG OIL PRESS REMAINED AT ZERO OIL QTY INDICATED 12 QTS. REMOVED AND REPLACEDSDR FDEA2019112213022Floorbeam · corrodedMAIN CABIN STA 1681 LBL 39/40 FLOOR BEAM UPPER T-CAP IS CORRODED REMOVE DAMAGE AND REPAIRED IAW FEDEX EA# F-5310-T0350636SDR FDEA201911192995Web · corrodedCABIN FLOOR WEB CORRODED BS 1681, BL 11L -BL47L REMOVED DAMAGE AND REPAIRED IAW B757-200 SRM 53-60-51-2R AND EA# F5310-T0350636SDR FDEA201911162967Seal Depressor · gougedMCD CUT OUT FWD SEAL RETAINER IS GOUGED - DOT & STREAMER ATTACHED REMOVED, FABRICATED AND REPLACED SEAL DEPRESSOR IAW B757 DWG 69-34527 AND DWG DWG 143N8730 REV ASDR FDEA2019111542962Frame · dentedAFT PIT FRAME BENT B.S.1420 BETWEEN STR 23L AND 24L. BS1420, STR 23L STR 24L REPAIRED FRAME AT STA 1420 STR23L-STR24L IAW FDX E.A.#F-5310-T0350569SDR FDEA2019111542961Plate · cracked#1 ENG O/B CORE COWL L/E PLATE CRACKED AT LWR END REMOVED AND REPLACED FILLER PER FEDEX EA # F7110-T0350560P1SDR FDEA201911122926Skin · damagedEXTERNAL SKIN DOUBLER REPAIR IS GOUGED IN 2 PLACES AND DENTED AT FASTENER HOLE BS 418-BS 419,STR 17 LEFT SIDE AFT OF L1 DOOR REMOVED AND REPLACED DOUBLER PER B757 SRM 53-00-01-2RSDR FDEA2019111522926Skin · gougedEXTERNAL SKIN DOUBLER REPAIR IS GOUGED IN 2 PLACES AND DENTED AT FASTENER HOLE BS 418-BS 419,STR 17 LEFT SIDE AFT OF L1 DOOR REMOVED AND REPLACED DOUBLER PER B757 SRM 53-00-01-2RSDR FDEA2019111102916Rub Strip · cracked#1 ENG O/B REV T/E LWR CHAFE STRIP CRACKED REMOVED AND REPLACED CHAFE STRIP PER EA # F-7830-T0350620-P1SDR FDEA2019110762897Bracket · broken#1 ENG O/B REV T/E BRACKET BROKEN STREAMER ATTACH REMOVED AND REPLACED BRACKET AT #1 ENG O/B REV T/E PER BAC DWG # 315N3105 REV CATCHR AND B757 SRM 51-40-02SDR FDEA2019110752872Floorbeam · crackedMAIN CABIN STA 1640 AT APPROX RBL 45 FLOOR BEAM SUB-STRUCTURE IS CRACKED VIEWED FROM BELOW (STREAMER ATTACHED) REPAIRED STA 1640 @ RBL 45 FLOOR BEAM SUB STRUCTURE STRAP PER B757 53-00-51-2RSDR FDEA2019110752871Web · corrodedCABIN FLOOR WEB CORRODED BS 1640 - BS 1653, BL 54R - BL-58R REPAIRED FLOOR WEB AT STA BS1640-1653, BL 54R-58R IAW B757 SRM 53-60-15-1A AND B757 SRM 51-20-01-0GSDR FDEA2019110752870Web · corrodedCABIN FLOOR WEB CORRODED BS 1642 - BS 1649, BL 57L REPAIRED FLOOR WEB AT BS 1642-1649 BL 57L IAW B757 SRM 53-60-15-1A AND B757 51-20-1-0GSDR FDEA2019110752868Web · corrodedCABIN FLOOR WEB CORRODED BS 1712, BL 0 REPAIRED FLOOR WEB AT B1712,BL0 IAW B757 SRM 53-60-51-1A AND B757 51-20-01-06SDR FDEA201911032851Access Panel · crackedR/W #9 SLAT AFT FACE I/B OF ACCESS PNL 624CB FASTENER HOLE POSSIBLE CRACK FABRICATED NEW PANEL PER DWG # 114N4076SDR FDEA201911022830Bracket · bentMAIN CARGO OVER WING AREA AT BS 1088 LBL55 BRAVKET BENT FABRICATED NEW BRACKET PER BAC DWG# 287N4407 REV T AND INSTALLED NEW BRACKET PER BAC DWG# 287N4407 REV F AND B757 SRM 51-40-02SDR FDEA201910302788Nut Plate · corrodedMAIN CABIN 1681 APPROX LBL 12 NUTPLATE STRIP UNDER THE FLOOR BEAM UPPER CAP IS CORRODED REMOVED CORRODED NUTPLATE STRAP, REMOVED CORROSIONUNDER STRAP, TREATED BARE METAL, FABRICATED NEW STRAP INSTALLED IAW B757-200 SRM 51-40-02, SRM 51-20-01, S SRM 53 SDR FDEA201910302787Nut Plate · corrodedMAIN CABIN STA 1681 APPROX RBL 11.5 NUTPLATE STRIP UNDER THE FLOOR BEAM UPPER CAP IS CORRODED REMOVED CORRODED NUTPLATE STRAP, REMOVED CORROSION UNDER STRAP, TREATED BARE METAL, FABRICATED MEW STRAP, INSTALLED B757-200 SRM 51-40-02, SRM 51-20-01,SRM 53-6SDR FDEA201910302786Nut Plate · corrodedMAIN CABIN STA 1681 APPROX RBL 24 NUTPLATE STRIP UNDER THE FLOOR BEAM UPPER CAP IS CORRODED REMOVED CORRODED NUTPLATE STRAP , REMOVED CORROSION UNDER STRAP,TREATED BARE METAL, FABRICATED NEW STRAP INSTALLED IAW B757 SRM 51-40-02, SRM 51-20-01, SRM 53-60SDR FDEA2019102872762Floor Support · corrodedCABIN FLOOR INTERCOSTAL CORRODED BS1675,BL 0 REMOVED AND REPLACED INTERCOSTAL PER B757 SRM 51-40-02 AND DWG # 146N5576SDR FDEA201811283389Placard · loosePOST FLIGHT L1 DOOR SLIDE ARM/DISARM CONDITION INDICATOR RED/GREEN PLACARD LOOSE. RESECURED L1 DOOR ARM/DISARM CONDITION INDICATOR PLACARD, DOOR ARM/DISARM OPS CHK OK.SDR FDEA201608232959Light · inoperativeEMERGENCY SLIDE LIGHT FO R1 PASSENGER DOOR INOPERATIVE. REPLACED BULB.SDR FDEA201512013836Fire Warning · false activationMAIN CARGO FIRE WARNING ILLUMINATED AT APPROX 100 KNOTS ON TAKEOFF ROLL. REJECTED TAKEOFF ACCOMPLISHED & QRH CONSULTED. CRASH & FIRE RESCUE RESPONDED, NEGATIVE INDICATION. BRIEFED CREW AT BLOCK IN, CARGO FIRE WARNING ALERT EXTINGUISHED AFTER EXITING RUNWAY.SDR FDEA201509262964Doubler · missingBONDED DOUBLER REPAIR MISSING, RT HORIZONTAL STABILIZER UPPER SKIN NEAR LE, APPROX 24" FROM INBD END OF STABILIZER. REPAIRED IAW IAW SRM 55-10-01-1A FIG 101 & SRM 51-70-10-2R REPAIR NR 4 & PARAGRAPH 11 20 7 OF SRM 51-70-10-2R.
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