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 FDEA202107161796Skin · delaminatedR/W L/E HAS EVIDENCE OF BEING DALAMINATED AFT OF #8 SLAT REPAIRED PER B757 SRM 57-41-01-2R AND 51-70-07-0G PARA 4CSDR FDEA202107151786Rib · crackedR/W L/E RIB OSS 515.32 FWD HOLE IS CRACKED REPAIRED PER FEDEX EA # F-5720-T0362806-P1SDR FDEA202107141779Frame · crackedSTA 1640 LH SIDE AT S14L CRACK INDICATION IN LOWER INB HOLE, IN THE FRAME LAYER ACCOMPLISHED FEDEX EA# F-5310-T0362516-P1 FUSELAGE - MAINFRAME - FRAME WEB, STA 1640 S-14L, CRACK INDICATION*THIS EA DEVIATES FROM EO F-5310-E0344602SDR FDEA202107131766Rib · crackedL/W L/E RIB FSS 213 IS CRACKED REPAIRED PER FEDEX EA # F-5720-T0362818-P1SDR FDEA202107121753Plate · crackedR/W T/E REAR SPAR WIGGLE PLATE IS CRACKED BENEATH #8 SPOILER REMOVED AND REPLACED PER BOEING DWG #113N1630 REV BSDR FDEA202107121752Attach Angle · crackedR/W L/E STRUCTURE FSS 560 ATTACH ANGLE IS CRACKED REMOVED AND REPLACED ANGLE PER DWG #114N2034 REV CSDR FDEA202107111724Panel · crackedLEFT WING, OUTBOARD AILERON, PCU HINGE PANEL IS CRACKED AT OUTBOARD PCU. REPAIRED L/W, OUTBOARD AILERON, PCU HINGE PANEL CRACKED AREA IAW BOEING 757- SRM 57-51-04-OI, ,51-70-05-OG 5.A, 57-51-01-2R FIG 201 SHEET 3.SDR FDEA202107061696Skin · dentedL/H WING O/B AFT FLAP HAS 1EA DENT AT UPPER SURFACE APPROX 27" O/B OF THE 2ND TRACK OF THE AFT FLAPAND 9.25" FROM THE T/E REPAIREDL/W O/B AFT FLAP DENT AT THE UPPER SURFACE APPROX. 27" O/B OF THE 2ND TRACK OF THE AFT FLAP AND 9.25" FROM THE T/E IAW B757 SRSDR FDEA202107061695Skin · dentedL/H WING O/B AFT FLAP HAS 1EA DENT AT UPPER SURFACE APPROX. 13" I/B OF THE 2ND TRACK OF THE AFT FLAP AND 5" FROM THE T/E. REPAIREDL/W O/B AFT FLAPDENT AT THE UPPER SURFACE APPROX. 13" I/B OF THE 2ND TRACK OF THE AFT FLAPAND5" FROM THE T/E IAW B757 SRM: 57-SDR FDEA202107061694Skin · dentedL/H WING O/B AFT FLAP HAS 1EA. DENT AT UPPER SURFACE APPROX 2" FROM THE I/B SIDE AND 5" FROM THE T/E. REPAIRED L/W O/B AFT FLAP DENT AT UPPER SKIN APPROX. 2" FROM THE I/B SIDE AND 5" FROM THE T/E IAW B757 SRM: 57-53-01, 51-70-04-0G AND AMM 51-21-00/701 RESDR FDEA202107061693Skin · delaminatedRIGHT WING UPPER L/E I/B SKIN IS DELAMINATED AFT OF #6 SLAT REPAIRED PER SRM 57-41-01 FIG 201SDR FDEA202107021661Web · corrodedNOSE GEAR RIGHT SIDE TUNNEL AREA WEB LOWER SURFACE HAS CORROSION AT BS320 STR17R AS MARK. REMOVED .003" CORRODED MATERIAL FROM ORIGINAL .040" MATERIAL THICKNESS. REMAINING .037" MATERIAL THICKNESS FOUND TO BE WITHIN LIMITS IAW B757 SRM 53-10-15-1A. APPLISDR FDEA202107021660Scuff Plate · crackedL4 DOOR CUTOUT, FWD CORNER SECTION SCUFF PLATE IS CRACKED. REMOVED AND REPAIR AREA IAW FEDEX DWG NO- SR57-53-003 REV A. REINSTALLED SCUFF PLATE IAW AMM 53-13-01-4.SDR FDEA202107021659Rub Strip · crackedR/W I/B FLAP O/B SUPPORT CARRIAGE I/B AND O/B PHENOLIC RUB STRIPS ARE CRACKED REMOVED AND REPLACED RUB STRIPS PER DWG #113N2150 REV CSDR FDEA202104080851Skin · damagedDURING AGING AIRCRAFT INSPECTION OF EXISTING REPAIR LOCATED ON FUSELAGE SKIN AT STA 1380 STR 14L FOUND MULTIPLE TOOLING MARKS ON REPAIR DOUBLER ACCOMPLISHED FEDEX EA F-5330-T0309534-P6 FUSELAGE - PLATES AND SKINS - LOWER SKIN PANEL CORROSION AND DENT REPAISDR FDEA202104020811Door · bent#1 PYLON I/B DOOR PANEL 443LL BENT OUT AT TOP AFT CORNER REPAIRED ACCESS DOOR IAW B757 SRM 54-50-01 SHEET 1 AND 51-70-08-2R FIG 5SDR FDEA202012223194Slide · dislodgedAFTER COMPLETING PREFLIGHT WHILE CLOSE R-1 DOOR FOUND GIRT BAR HANGING OUT. OPENED DOOR AND FOUND SLIDE FELL OUT OF DOOR. MEL 22DEC20 00:27 FNT U. RELEASED FOR SERVICE, PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 25DEC20 "MEL 52-11-01-A: R1 DOOR OR SLIDE-RESDR FDEA202012183188Crank Assy · brokenWHILE PERFORMING MEL VERIFICATION FOR MEL 25-66-05-A WRI 8405. FOUND GIRT BAR IS NOT ENGAGING. SUSPECT BAD LINKAGE. VERIFIED SLIDE LIGHT COMES ON WHEN WHEN PLACING MAGNETS OVER SENSOR NEAR FOOT RETAINERS, REF AMM 25-66-11-2. R1 DOOR SLIDE IS INOPERABLE. FSDR FDEA202012153158Crank Assy · inoperativeR-1 DOOR ARMING LIGHT INOPERABLE WHILE PERFORMING MEL VERIFICATION FOUND GIRT BAR IS NOT ENGAGING. SUSPECT BAD LINKAGE. VERIFIED SLIDE LIGHT COMES ON WHEN WHEN PLACING MAGNETS OVER SENSOR NEAR FOOT RETAINERS, REF AMM 25_66_11_2 AMM 25-66-04-4, CMM 52-11-05. SDR FDEA202010202564Sensor · failedON TAXI OUT, LT FWD ENTRY DOOR EICAS MESSAGE WITH ASSOCIATED DOOR LIGHT ILLUMINATED OPENED/SHUT DOOR, CONDITION REPEATED. REMOVED AND REPLACED LT DOOR SENSOR, PER MM 52-71-00-4. OPERATIONS CHECKS GOOD. OPENED AND CLOSED DOOR SEVERAL TIMES WITH NO FAULTS. RSDR FDEA202009012077Wheel · damagedPDIS 997 32-41 8143 01SEP20 MEM OPEN U. DURING TAXI IN OBSERVED ABNORMAL SOUND AND VIBRATION FROM LANDING GEAR/TIRES/WHEELS. SET BRAKE, SHUTDOWN, COORDINATED TOW IN TO GATE. SHGN 01SEP20 08:55 MEM U. THE LEFT NOSE TIRE, WHEEL HUB/WHEEL ASSY HALVES ARE BRSDR FDEA202007171559Receptacle · damagedR1 DOOR WILL NOT ARM AND SLIDE LIGHT WILL NOT ILLUMINATE. FOUND R1 DOOR GIRT BAR ANNUCIATOR LIGHT RECEPTACLE L404 PIN 2 READING ZERO VOLTS. REMOVED AND REPLACED THE RECEPTACLE L404 IAW IAW SWPM 20-84-00. NO OTHER DEFECTS NOTED. DOOR ARMING OPS NORMAL.SDR FDEA2020070871458Girt Bar · bindingL1 DOOR OPENS NORMALLY WITH THE HANDLE TO THE 2 O'CLOCK POSITION. VERY DIFFICULT TO MOVE THE HANDLE PAST 2 O'CLOCK POSITION TO THE LEFT- FULLY OPEN. FOUND L1 DOOR GIRT BAR JAMMED- RMVD AND RPLD GIRT BAR- DOOR OPENS AND CLOSES NORMAL AND ARMS AND DISARMSSDR FDEA2020071031416Slide · low pressureL1 RAFT BATTERY GAUGE IN DOOR OUT OF GREEN BAND. REPLACED THE L1 DOOR SLIDE RAFT IAW AMM 25-66-01-4. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA202006301394Battery · dischargedL1 RAFT BATTERY GAUGE IN DOOR OUT OF GREEN BAND. REPLACED L1 DOOR SLIDE RAFT IN REF TO AMM 25-66-01-4. OPS CHECK GOOD. AC OK FOR SERVICE. REMOVED SLIDE RAFT: PN D30654-122. SN 2055RP.SDR FDEA2020070201416Battery · dischargedL1 RAFT BATTERY GAUGE IN DOOR OUT OF GREEN BAND.SDR FDEA2019082071925Panel · crackedFOUND CRACK ON UPPER AFT O/B FIXED WING PANEL. WHERE THE SKIN PANEL 112N3501-5 ATTACHES AT I/B AFT CORNER. REF WRI 57-20/7350. REMOVED PANEL 113N1640-31 FROM OUTBD END OF UPPER LEFT WING FOR REPAIR. THE DAMAGE IS APPROX 1' LONG ON EDGE LAND APPROX 61" FROM SDR FDEA2019080281790Skin · damagedDELAMINATION ON L/H OUTER WING SKIN AT PANEL 112N3501. DAMAGE IS APPROX. BETWEEN WS 813.50 & WS 830.00. DAMAGE AREA IS 16.4IN LENGTH, 13.50 WIDTH. COMPLIED WITH PART 1 OF EA F-5710-T0348642.SDR FDEA2019061321280Floorbeam · corrodedFLOOR BEAM AT STA.377 FWD FLANGE HAS CORROSION FROM LBL.25-LBL.58 COMPLIED WITH FEDEX EA#F-5310-T0347236 P1, STA.377 FLOOR BEAM UPPER FORWARD FLANGE REPAIR BETWEEN LBL.24 ABD LBL.58.SDR FDEA2019061321276Floorbeam · corrodedFLOOR SUPPORT AT STA.376, LBL.10 - LBL. 24 HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS, 100% MATERIAL LOSS ON FLOOR SUPPORT AT STA.376 LBL.10 TO LBL.24 IAW B757 SRM 53-00-51-1A, REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT FROM 2024-T3 ..071,SDR FDEA2019060641225Floorbeam · corrodedMAIN CABIN STA 333.45 BETWEEN LBL 45.5 - LBL 58.22 FLOOR SUPPORT CORRODED. REMOVED CORR ON FLOOR SUPPORT (STUB BEAM) WITH 100% MAT LOSS OUT OF LIMITS FABRICATED AND INSTALLED NEW SUPPORT (STUB BEAM) AT STA 333.45 LBL 45.5 TO LBL 69.10 IAW DWG 141N5110 REV SDR FDEA2019052861172Floorbeam · corrodedMAIN CABIN R/H SIDE FLOOR T CHORD AT RBL.45 STA.324. REMOVED CORR. IN MAIN CABIN T CHORD STA.324 RBL.45. ORIG MAT.120, LOSS .042, REMAIN. .078 OUT OF LIMITS, CUT OUT DAMAGED SECTION OF T CHORD FROM RBL.32 TO RT OB END AND INSTALLED REPAIR SECTION.IAW B757 SDR FDEA2019052861170Floorbeam · corrodedMAIN CABIN STA.365 BETWEEN RBL.15 - RBL.47 CORROSION ON FLOOR BEAM T CHORD. UPON FURTHER EVALUATION FOUND CORR. ON "T" CHORD STA.365 RBL.15 - RBL.47 TO BE OUT OF LIMITS DUE TO CORR. BEING ON EXISTING REPAIR. REMOVED AND REPLACED "T" CHORD SECTION OF EXISTISDR FDEA2019052861171Floorbeam · corrodedMAIN CABIN STA.1200 BETWEEN BL.0- LBL.24.5 FLOOR BEAM T CHORD CORRODED. REMOVED CORR. IN MAIN CABIN FLOOR BEAM STA.1200 BL.0 -LBL.24.5. ORIG. THICKNESS .125" LOSS .028 ,REMAIN. .093 OUT OF LIMITS , CUT OUT DAMAGED SECTION OF UPPER CAP OF FLOOR BEAM RBL.10 SDR FDEA201905191096Floorbeam · crackedMAIN CABIN FLOOR STRUCTURE-STA.580 STUB FLOORBEAM AT LBL 45.5 HAS A CRACK ON AFT FLANGE AS SEEN FROM FWD CARGO COMPARTMENT. COMPLIED WITH EA F- 5310-T0347001 P1, FUSELAGE - MAIN FRAME - STA. 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.SDR FDEA201810303055Iru · inoperativeON CLIMB OUT FROM CAE MULTIPLE EICAS HDG, ATT L-IRU, NO AUTOPILOT, PITCH AND ROLL FLAGS ON F/O'S WITH NO FMA'S. NO AUTO BRAKES ON LAND, SPLIT IRS. IDENTIFIED PARTS IRU WITH 2005 &/OR 2015 M MPN: HG1050AC15 CPN: 3416054 QTY 1. RIGHT IRU INOP. VERIFY AND RECORD SDR FDEA201805151235Landing Gear · malfunctionedGREEN RIGHT MAIN GEAR LIGHT, EICAS FOR GEAR DISAGREE, AND GEAR DOOR ANNUNCIATOR, WHEN THE HANDLE WAS SELECTED OFF, AFTER TAKE OFF. LIGHTS EXTINGUISHED WITH A NOTICABLE CLUNK FROM GEAR OR DOORS WHEN HANDLE MOVED TO UP POSITION IAW QRH, CLUNK WAS HEARD AFTSDR FDEA201801170105Girt Bar · dirtyL1 DOOR ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. INSPECTED THE L1 DOOR SLIDE GIRT BAR IAW AMM. FOUND THE GIRT BAR LINKAGE WITH BUILD UP OF DIRT. CLEANED AND REMOVED. SLIDE ARMS NORMALLY WITH NORMAL LIGHT INDICATISDR FDEA201708012087Sequence Valve · malfunctionedAFTER TAKEOFF, FOLLOWING POSITIVE RATE GEAR UP CALL, DOORS GEAR REMAINED ON PAST NORMAL CLEANUP. EICAS MESSAGE FOLLOWED UP WITH GEAR DISAGREE AND GEAR DOORS, FLT CREW FOLLOWED QRH, LEVELED AT 5000 MSL. AIRCRAFT ACCELERATED TO 250 K. AS FELT PHYSICAL MESDR FDEA201707202006Sequence Valve · leakingFOLLOWING GEAR UP CALL, HANDLE UP, DOORS, GEAR DISAGREE LIGHTS ILLUMINATED, GEAR DISAGREE EICAS MESSAGE FOLLOWED. CLEANED UP A/C ON SCHEDULE ACCELERATED TO 250 KIAS, A/C CONFIGURATION CLEAN BY 5900 MSL, DISAGREE LIGHTS AND MESSAGES EXTINGUISHED. PSEUSDR FDEA201707191992Actuator · inoperativeRT MAIN LANDING GEAR DID NOT RETRACT ON TAKEOFF. TOWER NOTIFY. RECIEVED A GEAR DISAGREE EICAS MESSAGE. GEAR CAME UP AT 15K. REMOVED AND REPLACED RIGHT MAIN GEAR TRUCK POSITIONER ACTUATOR. OPS AND LEAK CHECK NORMAL. GEASDR FDEA201705091380Frame · gougedFWD ACCESSORY BAY, LOWER FUSELAGE FRAME, BS 231 BL 0 HAS GOUGE IN THE RADIUS. REPAIRED IAW EA F-5310-T0333062, P1.SDR FDEA201704121159Oil System · lowDURING APPROACH, WHEN SELECTING FLAPS 25 RECEIVED EICAS TE FLAPS DISAGREE, RAN QRH AND DECLARED AN EMERGENCY. MADE FLAPS 20 LANDING. INSPECTION REVEALED LEFT INBD TE FLAP OTBD TRANMISSION REQUIRED SERVICEING DUE TO SHOWING MINIMAL OIL IN SIGHT GLASS. ASDR FDEA201703210966Warning Message · false activationLEADING EDGE SLAT DISAGREE. RAN QRH. EXTENDED FLAPS WITH ALT FLAP SWITCH. TROUBLESHOT IAW FIM 27-81 FT 803. PERFORMED FSEU BITE IAW FIM 27-51 FT 803, FIG 104. NO FAILURES FOUND. SLAT SECURITY CHECKED GOOD. OPERATED SLATS THROUGH SEVERAL CYCLES WITH NO FASDR FDEA201509032768Cover · looseL1 SLIDE RAFT COVER IS LOOSE. ADJUSTED LOWER CTR LATCH STRAP. SLIDE COVER OK FOR SERVICE IAW MM 52-11-02-4.SDR FDEA201507092185Connector · looseFLIGHT COMPARTMENT EMER DOME LIGHT WILL NOT ILLUMINATE DURING TEST. SPLICE CONNECTOR AT D5264 IS LOOSE. RESEATED SAME & FLIGHT DECK EMER LIGHT OPERATIONS CHECKED NORMAL.SDR FDEA201506252043Hydraulic Line · leakingWHILE ON FINAL APPROACH TO 18L JUST PAST, RONEE RCVD, DOORS CAUTION ON LG INDICATION PANEL. FOLLOWED QRH & ELECTED TO LAND. AT APPROX 3 MILES RCVD EICAS MSG, LT HYD QTY, FOLLOWED BY OTHER INDICATIONS OF HYD SYS FAILURE. ELECTED TO LAND, USED DIFFERENTIAL BRSDR FDEA201505071403Shear Tie · crackedSHEAR TIE CRACKED BS 1300 BETWEEN STRINGERS 19 & 20R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, DWG 140N2002 REV EU, SRM 51-30-01 SRM 51-40-02, DWG 140N2002 REV EU AND DWG 146N1006 REV B.SDR FDEA201503241071Strap · looseL1 ENTRY DOOR VERY DIFFICULT TO CLOSE & LOCK. FOUND SLIDE COVER LOOSE ON L1 ENTRY DOOR. TIGHTEN STRAP ON SLIDE COVER IAW AMM 25-66-01-4. OPENED & CLOSED L1 ENTRY DOOR SEVERAL TIMES WITHOUT ANY PROBLEMS. OPERATIONS CHECKED GOOD IAW AMM 52-11-00-6.SDR FDEA201503190992Warning System · false activationRT SLIDE EICAS DURING CONFIGURATION FOR APPROACH, REPEAT. PERFORMED INSPECTION & CHECK OF THE R1 PAX DOOR ESCAPE SYS IAW MM 25-66-01-6. NO DEFECTS NOTED, ACFT OK FOR SERVICE.
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