N997FD
Service difficulty reports · 158
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 = 'N997FD' 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 = 'N997FD' 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 FDEA202610021467Door Latch · out of adjustPASSING THROUGH 17000FT THE FWD ACCESS DOOR EICAS APPEARED ALONG WITH THE ACCESS DOOR OVERHEAD LIGHT. THE AIRCRAFT BEGAN TO DEPRESSURIZATION SIMULTANEOUSLY. WE RAN THE QRH PROCEDURE AND LANDED UNEVENTFULLY. AMM: 52-48-01-4. ADJUSTED FWD ACCESS DOOR LATSDR FDEA202605280642Gust Lock · brokenL1 DOOR GUST LOCK BROKEN. REMOVED BROKEN PIECES OF GUST LOCK, BAGGED AND PLACED IN GALLEY COMPT WITH 02 DEMO MASK. NO ADDITIONAL DAMAGE FOUND. RELEASED FOR SERVICE PER MEL : 52-11-01-A COMPLIED WITH MEL PROCEDURES. A/C OK FOR SERVICE. REMOVED AND REPLASDR FDEA202603110333Bulb · dimDURING MX PRE-FLIGHT FOUND L1 EMERGENCY EXIT SIGN DIM. REMOVED AND REPLACED 8 FAULTY BULBS AT THE L1 EMERGENCY EXIT SIGN AS PER ABOVE REF. OPS CHECK GOOD. ACFT OK FOR SERVICE.SDR FDEA202602100170Indicator · damagedAT BLOCK IN , FOUND R1 DOOR SLIDE RED-GREEN, ARM-DISARM LEVER INDICTOR FALLING OUT OF PLACE. REMOVED INDICATOR PLACED IN GALLEY AREA STOWAGE. RELEASED FOR SERVICE PER MEL 25-66-04-A, CATEGORY C, R1 DOOR ESCAPE SLIDE ARMED INDICATORS INOP. REMOVED R1 DOOR USDR FDEA202509111684Girt Bar · out of alignmentL1 DOOR SLIDE WILL NOT ARM. AFT SECTION OF GIRT BAR WILL NOT ALIGN OR ENTER DOOR FRAME CHANNEL. RELEASED FOR SERVICE PER MEL 52-11-01-A CATEGORY : B. FOUND STATIC LINE AND SPRING SNAP REMOVED FROM POUCH AND LODGE UNDER GIRT BAR AND PREVENTING GIRT BAR FROM SDR FDEA202507171231Cylinder · emptyAFTER SLIDE REINSTALLED NOTED L1 DOOR EMERGENCY POWER RESERVOIR EMPTY. REMOVED AND REPLACED L1 DOOR EMERGENCY POWER RESERVOIR WITH REF AMM 52-11-30-4. A/C OK FOR SERVICE.SDR FDEA202507131186Slide · warning messageRIGHT WING SLIDE EICAS ON TAXI OUT. TERMINATING ACTION ACCOMPLISHED FOR E.A. F-5220-T0384096. INSTALLED 4EA SEALING BOLTS FOR THE OVERWING SLIDE PANEL. INSTALLED ACCESS PANEL IN THE AFT OUTBOARD CORNER OF THE RIGHT MLG BAY REFERENCED BY THE ABOVE MAINTENANCSDR FDEA202410101473Door · delaminatedLH LANDING GEAR FLYING DOOR HAS POSSIBLE DELAM REMOVED AND REPLACED L/H GEAR FLYING DOOR PER B757 MM 32-12-04-4 AND ADJUST AND TEST B757 AMM 32-12-00-5 . OPS CHK GOODSDR FDEA202407311075Controller · faultedAT FL390 APPROXIMATELY 20 MINUTES AFTER LEVEL OFF RECEIVED CABIN ALTITUDE WARNING. CABIN ALTITUDE READ 10,000 AND SLOWLY INCREASED TO APPROXIMATELY 12,000 . OXYGEN MASKS WERE DONNED. CABIN ALTITUDE REMAINED ABOVE 10,000 UNTIL DESCENDING THRU APPROXIMATELSDR FDEA202407161024Slide · detachedDURING WALK AROUND FOUND R1 DOOR OPEN AND R1 SLIDE DISCONNECTED FROM R1 DOOR REINSTALLED R1 SLIDE /RAFT AND OPS CK AS NEEDED REF M/M 25-66-01-4 ACFT OK FOR SERVICESDR FDEA202407090974Gust Lock · crackedPOST-FLT INSPECTION, FOUND L1 DOOR HOLD-OPEN LOCK BROKEN. LINE MEL 09JUL24 07:07 MEM RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B MEL 52-11-01-A: L1 DOOR INOP. L1 DOOR HOLD-OPEN LOCK FOUND BROKEN. REMOVED BROKEN SPLIT LOCK PIECES AND PLACEDSDR FDEA202308021348Selector Panel · damagedLEVELING OFF AT FL350, CABIN ALT MC. CABIN ALT NOTED 12,000 . AFTER QRH PROCEDURES AND LEVELING AT 10,000 , CABIN AUTO INOP MW. AIR TURN BACK TO MEMPHIS. EMERGENCY DECLARED. UPON FURTHER TROUBLE SHOOTING FOUND THAT OUTFLOW VALVE INDICATION ON CABIN PRESSSDR FDEA202305300976Battery Pack · failedLH EMERGENCY LIGHTS INOP REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PAXK (M731) B757 AMM 33-51-07-2SDR FDEA202305270967Unknown · unknownAGING AIRCRAFT INSPECTION, FOUND ADDITIONAL REPAIR NOT PREVIOUSLY RECORDE/ACCOUNTED FOR IN OPERATORS RECORDS; EXISTING REPAIR IS LOCATED ON FUSELAGE EXTERNAL SKIN APPROX. STA 1385 AND S3L ACCOMPLISHED FEDEX EA# F-5330-T0374359: FUSELAGE - PLATES & SKINS - SDR FDEA202305250940Skin · unknownDURING AGING AIRCRAFT INSPECTION, FOUND EXISTING REPAIR LOCATED ON FUSELAGE EXTERNAL SKIN, STA 1570 TO STA 1585, S3L TO S5L, REQUIRES EVALUATION FOR B757-200SF LOADING COMPLIED WITH FEDEX E.A. F-5330-T0374381-P1, TITLE: FUSELAGE - PLATES AND SKINS - BS 157SDR FDEA202305250938Skin · unknownDURING AGING AIRCRAFT INSPECTION, FOUND EXISTING REPAIR LOCATED ON FUSELAGE EXTERNAL SKIN, STA 1495 TO STA 1522, S3L TO S5L REQUIRES EVALUATION FOR B757-200SF LOADING COMPLIED WITH FEDEX E.A. F-5330-T0374384-P1, TITLE: FUSELAGE - PLATES AND SKINS - BS 1495SDR FDEA202305230922Spar · corrodedL. WING O/B MAIN FLAP FRONT SPAR LOWER CHORD IS CORRODED. ACCOMPLISHED REPAIR OF L.WING O/B MAIN FLAP FRONT SPAR LOWER CHORD PER FEDEX EA # F-5750-T0374247-P1 TITLE: WINGS - FLIGHT SURFACES - LH OUTBD MAIN FLAP, FWD LOWER SPAR CHORD, AFS564, CORROSION REPAISDR FDEA202305230921Access Panel · corrodedLEFT WING FUEL TANK ACCESS PANELS 541FB, 541JB, 541DB, 542BB AND 543AB ARE CORRODED REMOVED AND REPLACED CORRODED FUEL TANK PANELS WITH NEW PANELS PER BAC DWG 112N6101SDR FDEA202305230920Access Panel · corrodedRIGHT WING FUEL TANK ACCESS PANELS 641EB, 642AB, 642BB, 641DB, 641GB, 641KB, 641LB SMF 642FB HAVE CORROSION. REMOVED AND REPLACED FUEL PANELS WITH NEW FUEL PANELS PER BAC DWG 112N6101SDR FDEA202305190904Panel · delaminatedDURING AGING AIRCRAFT INSPECTION FOUND EXISTING REPAIR LOCATED ON THE VERTICAL STABILIZER L/H SIDE SKIN PANEL (P/N 175N2003-19) DOES NOT CONFORM TO CURRENT DOCUMENTATION AND SRM REPAIR REFERENCED. REPAIR IS METAL BONDED DOUBLER AND SRM REFERENCED IS FOR COSDR FDEA202305180898Retainer · corrodedL/H WING #1 SPOILER HAS CORRODED SEAL RETAINER 4TH RETAINER FORM THE I/B EDGE REMOVED AND FABRICATED NEW SEAL RETAINER AND REINSTALLED PER B757 SRM 51-40-02 AND BAC DWG 113N5100 REV CSDR FDEA202305180897Retainer · corrodedL/H WING #1 SPOILER HAS CORRODED SEAL RETAINER 2ND SEAL RETAINER FROM I/B EDGE. REMOVED SEAL RETAINER, FABRICATED NEW SEAL RETAINER AND REINSTALLED PER B757 SRM 51-40-02 AND BAC DWG 113N5100 REV CSDR FDEA202305170891Skin · damagedRIGHT WING INBOARD LEADING EDGE DAMAGED AT AUX TRACK CUTOUT. PERFORMED PERMANENT REPAIR ON RIGHT WING INBOARD LEADING EDGE AT AUX TRACK CUTOUT IAW DX B757 SRM 57-41-01-2R FIG 201 SHEET 2 AND 51-70-08-0G.SDR FDEA202305160881Structure · corrodedAREA ABOVE CTR WING CORROSION AT NUT PLATES UNDER PANEL 241MDF EVALUATED & REMOVED CORR @ LBL 58 O/B STA 903 - 930 IAW SRM 53-00-52-1A, REMAINING MATL ON FLANGE IS .071 FOUND TO BE WITHIN LIMITS IAW BAC1520-792. REMOVED CORR @ LBL 64 STA 989 ORIG MATL .070,SDR FDEA202305160878Unknown · unknownAREA ABOVE CTR WING CORROSION AT NUTPLATES UNDER PANEL 241MAF ACCOMPLISHED FEDEX EA# F-5310-T0374303 : FUSELAGE - FUSELAGE - MAINFRAME - LONGITUDINAL FLOR BEAM, STA 1015,BL0, CORROSIONSDR FDEA202305150867Web · corrodedMAIN CARGO STA 1664-1682 SHEER WEB AT R4 DOOR LOWER SURFACE IS CORRODED REPAIRED PER FEDEX EA # F-5310-T0374304-P1SDR FDEA202305120864Filler · corrodedT-CHORD FILLER FOR UNDER WING TO BODY FAIRING IS CORRODED BETWEEN BS 900-BS 950 REMOVED AND REPLACED PER BOEING DWG # 149N7320 REV ESDR FDEA202305120863Strap · corrodedR/W O/B T/E FWD FLAP O/B UPPER SURFACE AT PANEL LAND IS CORRODED REPAIRED AREA PER FEDEX EA # F-5750-T0374318-P1SDR FDEA202305110859Unknown · unknownDURING AGING ARIRCRAFT INSPECTION, FOUND EXISTING FUSELAGE EXTERNAL REPAIR WITH ONE POPPED RIVET LOCATED AT APPROX. STA 1338 AND JUST BELOW S4LSDR FDEA202305110858Floorbeam · corrodedMAIN CABIN FLOOR BEAM HAS SURFACE CORROSION IN SEVERAL SPOTS UNDER FLOOR PANEL 221MBF NEAR GREEN COMPOUND IN FRONT OF CABIN TO CARGO DOOR. REPAIRED PER FEDEX EA# F-5310-T0347256SDR FDEA202305110856Rib · crackedCRACKED FASTENER HOLE SECOND FROM TOP FOUND ON R/H WING L/E RIB ISS 119.00 REPAIRED PER EA # F-5720-T0374308-P1SDR FDEA202305110855Rib · crackedCRACKED FASTENER HOLE SECOND FROM TOP FOUND ON R/H WING L/E RIB ISS 148.26 REPAIRED PER EA # F-5720-T0374308-P1SDR FDEA202305100841Panel · delaminatedL/WING IB FLAP LWR SURFACE OF CLOSE OUT FAIRING IS DELAMINATED. ACCOMPLISHED PERMANENT REPAIR OF DELAMINATION ON LOWER SURFACE OF L/W INBRD MAIN FLAP AFT FLAP CLOSE OUT IAW B757 SRM 57-53-01-2R FIG 201 SHEET 6 AND 51-70-07-0GSDR FDEA202305100839Seat Track · corrodedMAIN CABIN FLOOR SEAT TRACK HAS CORROSION IN FEW SPOTS UNDER FLOOR PANEL 222MAF. REMOVED AND REPLACED SEAT TRACK IAW B757 DWG 3504 REV-SDR FDEA202305100838Intercostal · corrodedMAIN CABIN FLOOR BEAM UNDER L1 DOOR PAN ALONG FULL LENGTH HAS SURFACE CORROSION IN SEVERAL SPOTS UNDER FLOOR PANEL AREA 221MBF. REMOVED AND REPLACED INTERCOSTAL IAW B757 DWG 141N8322 REV KSDR FDEA202305100837Intercostal · corrodedMAIN CABIN FLOOR BEAM UNDER 1R DOOR DRAIN OAN ALONG FULL LENGTH HAS SURFACE CORROSION IN SEVERAL SPOTS UNDER FLOOR PANEL 222MAF. REMOVED AND REPLACED INTERCOSTAL IAW B757 DWG 141N5160 REV CDSDR FDEA202305090835Skin · delaminatedDURING INSPECTION, FOUND EXISTING SKIN REPAIR AND SURROUNDING AREA DELAMINATED ON THE LW O/B AFT FLAP UPPER SKIN, I/B END. ACCOMPLISHED PERMANENT REPAIR OF DELAMINATED SKIN ON THE INBRD UPPER SURFACE OF THE LEFT WING OTBRD AFT FLAP IAW B757 SRM 57-53-01-2SDR FDEA202305050814Doubler · crackedMAIN CABIN - L2 DOOR - UPPER HINGE CUTOUT HAS EVIDENCE OF CRACK. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW FED B757 SRM 52-10-02-2R REPAIR 1. REPAIR DOUBLER FABRICATED ON NR N00186.SDR FDEA202305030801Unknown · delaminatedDISBOND INDICATION FOUND ON UPPER SURFACE OF #8 SLAT, MOST OUTBOARD EDGE. REPAIRED #8 SLAT UPPER SURFACE IAW FEDEX EA # F-5750-T0374114-P1-FLIGHT SURFACES-#8 SLAT,TRAILING EDGE WEDGE, DELAMINATION-SRM REPAIR DEVIATION.SDR FDEA202305020795Stiffener · cracked#2 PYLON HYDRAULIC BAY FWD BULKHEAD UPPER STIFFENER ANGLE IS CRACKED IN THE CORNER. REMOVED AND REPLACED STIFFENER ANGLE PER BAC DWG 313N302 REV BSDR FDEA202304300782Nut Plate · corrodedMAIN CABIN PRESSURE DECK 2EA NUTPLATE STRAPS ARE CORRODED STA 1681 RBL4 TO RBL 12 REMOVED AND REPLACED PER BAC DWG #146N5693 REV BSDR FDEA202304260763Rub Strip · crackedR/H AFT WING TO BODY AFT RUB STRIP IS CRACKED. REMOVED AND REPLACED PER BAC DWG 149N7650 REV DSDR FDEA202304220772Wedge · corrodedL/H I/B MAIN FLAP HAS CORROSION AT THE TRAILING EDGE UPPER SURFACE FROM THE O/B SIDE TO 24" I/B. REPAIRED CORROSION ON LH IB MAIN FLAP TE WEDGE UPPER SURFACE 2 EA LOCATIONS 6" FROM OB EDGE AND 24" FROM OB EDGE IAW B757 SRM 51-10-02, SRM 57-53-01-1A, SRM 5SDR FDEA202304200774Panel · delaminatedL/W L/E PANEL 511HB IS DELAMINATED ON CORNER REPAIRED 2EA DELAMINATED CORNERS ON PANEL 511HB IAW B757 SRM 57-41-01-2R, AMD B757 SRM 51-70-08-0G. REPLACED EROSION STRIP IN REPAIR AREA IAW B757 SRM 57-41-01-2R REPAIR 2. REPLACED FOIL BACKING IAW BAC DWG 11SDR FDEA202304200723Unknown · unknownFUSELAGE SKIN AT STA 1600 - 1620 STR1R/2R DENTED. ACCOMPLISHED FEDEX EA# F-5330-T0374201: FUSELAGE - PLATES AND SKIN - STA 1609 -S-1 - S- 2R, DENT REPAIR DOUBLER.SDR FDEA202304180773Panel · delaminatedL. WING L/E PANEL 511DB IS DELAMINATED AND COMPOSITE DAMAGE ON THE CORNER REPAIRED DELAMINATION AND COMPOSITE DAMAGE ON LEFT WING L/E PANEL 511DB IAW B757 SRM 57-41-01-2R, 57-41-01-0I, 51-05-01, PART 1, 51-70-17-OG, AND 51-70-04-OG.SDR FDEA202304010537Controller · failedPDIS 997 21-30 0265 01APR23 TLH OPEN U CABIN ALTITUDE WARNING ALERT AT FL280 CABIN ALT AUTO 1 AN 2 FAILED COULD NOT GET CONTROL OF PRESSURIZATION . ***EMERGENCY DECLARED*** INFO 01APR23 04:12 MEM U ********************MOCC UPDATE**********SDR FDEA202206251561Engine · failedDURING CLIMBOUT L ENGINE OIL TEMPERATURE CLIMBED INTO THE AMBER BAND (167 DEGREES). ACCOMPLISHED QRH AND OIL TEMP REMAINED HIGH. SHUTDOWN ENGINE IAW WITH QRH INSTRUCTIONS AND LANDED SINGLE ENGINE WITHOUT ISSUE. EMERGENCY DECLARED. AFTER SHUTDOWN L ENG SECSDR FDEA202107181805Door Frame · gougedL1 DOOR CUTOUT ,FWD FRAME ,WEB I/B OF SNUBBER IS GOUGED REMOVED AND REPLACED WEB PER FEDEX EA # F-5310-T0362821SDR FDEA202107161797Skin · delaminatedL/W UPPER FIXED L/E I/B SKIN IS DELAMINATED IN TWO AREAS BEHIND #5 SLAT REPAIRED PER B757 SRM 57-41-01-2R-1 FIG 201 SHEET 6
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