N987FD
Service difficulty reports · 68
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 = 'N987FD' 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 = 'N987FD' 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 FDEA202601090017Skin · dentedRIGHT LOWER FUSELAGE BS 500 STRINGERS S21 TO S22 DENTED. COMPLIED WITH EA F-5330-T0386068 P1. FUSELAGE SKIN NICKS AND PREVIOUS BLENDOUT MARK BETWEEN STA 500 & STA 520, S-21R & S-22R.SDR FDEA202505050716Lamp · failedR1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. RELAMPED IAW ABOVE REF OPS CHK SERVICEABLE. OK TO CONTINUE.SDR FDEA202402190188Web · crackedTAIL COMPARTMENT STA 1862 RB8 UNDER AUTOPILOT SERVOS WEB IS CRACKED. FUSELAGE-MAINFRAME-STA 1862 BULKHEAD UPPER WEB CRACKED DUE TO CORROSION-WEB SPLICE AND CHORD STRAP REPAIR ACCOMPLISHED STEPS 1-8 PER EA-5310-T0377991 P1 WITH NO DEVIATION. MAJOR REPAIRSDR FDEA202402130155Floorboard · dentedMAIN DECK FOOR PANEL 251MWF HAS BROKEN AND CORRODED INSERTS FABRICATE ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER # T24/1733499 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIRSDR FDEA202305160880Holder · failedEMERGENCY EXIT LIGHT ABOVE R1 DOOR WONT TEST REMOVED AND REPLACED R/H EMERGENCY LIGHTS BATTERY PACK REF AMM 33-51-07-2SDR FDEA202206241543Relay · faulted2HRS INTO FLIGHT AT FL410, FWD AND AFT LEFT FUEL PUMPS BEGAN FLICKERING LOW PRESSURE VIA PRESS LIGHTS. OPENED THE CROSS FEED VALVES, LIGHTS EXTINGUISHED. A FUEL IMBALANCE QUICKLY BEGAN TO DEVELOP, MAX 1,300LBS. DESCENDED TO FL250 TO SUCTION FEEDSDR FDEA202203260696Skin · corrodedWHILE REMOVING APU INLET DUCT TO F.O.M. THE AFT SIDE OF CUT STRAP WAS FOUND EXFOLIATED. ACCOMPLISHED REPAIR IAW SRM 53-80-15-2R DETAIL I SHEET 2 ON AFT CUT OUT OF APU INLET AT STA. 1825 BETWEEN STRINGERS 5 & 6 FOR CORROSION DAMAGE ON STRAP PART # 148N3141-SDR FDEA202203250692Support · corrodedCORROSION FOUND BETWEEN STA 345.0 TO 365.0 AT BUTTLINE 0.0. REMOVED CORROSION BETWEEN STA 345.0 TO 365.00 BUTTLINE 0.0 IAW SRM 51-10-02. CHECKED LIMITS AFTER REWORK. DEPTH = 0.048" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A. REMOVED AND REPLACED FLOOR SDR FDEA202203250691Angle · corrodedAPU AIR INLET DOOR MANIFOLD ASSY RH SUPPORT ANGLE CORRODED. REMOVED AND REPLACED CORRODED ANGLE WITH A NEW ONE PART # 148N3152-1 BATCH # 0003918563 IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA202203230660Strap · corrodedWHILE REMOVING THE APU INLET DUCT TO F.O.M. CORROSION WAS FOUND ON THE FWD SIDE OF THE DUCT CUTOUT. REMOVED & REPLACED CORRODED STRAP ON APU INLET DUCT CUTOUT FWD STRAP WITH ONE FABRICATED ON TRAVELER T22/1605340 PART # FX148N3138-20 IAW SRM 51-40-02 & DRASDR FDEA202203100469Floorboard · delaminatedCOURIER AREA FLOOR BOARD 222MBF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222MBF FROM TRAVELER T22/1602811 IAW DWG SRZ- 25-005 REV. R."MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.SDR FDEA202203100468Floorboard · delaminatedCOURIER AREA FLOOR BOARD 222MCF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222MCF FROM TRAVELER T22/1602800 IAW DWG SRZ- 25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.SDR FDEA202203100467Floorboard · delaminatedCOURIER AREA FLOOR BOARD 222MDF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222MDF FROM TRAVELER T22/1602799 IAW DWG SRZ- 25-005 REV. R. "MAJOR REPAIR". PART MARKED IAW GMM 07-0-1001.SDR FDEA202203100466Floorboard · delaminatedCOURIER AREA FLOOR BOARD 222MEF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222MEF FROM TRAVELER T22/1602798 IAW DWG SRZ- 25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.SDR FDEA202203100465Floorboard · delaminatedCOURIER AREA FLOOR BOARD 222BF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222BF FROM TRAVELER T22/1602796 IAW DWG SRZ- 25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.SDR FDEA202203100464Floorboard · delaminatedCOURIER AREA FLOOR BOARD 222MAF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222MAF FROM TRAVELER T22/1602793 IAW DWG SRZ- 25-005 REV. R. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.SDR FDEA202203100463Floorboard · delaminatedCOURIER AREA FLOOF BOARD 222AF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 222AF FROM TRAVELER T22/1602792 IAW DWG SRZ- 25-005 REV. R. "MAJOR REPAIR" AND PART MARKED IAW GMM 07-0-1001.SDR FDEA202203100462Floorboard · delaminatedCOURIER AREA FLOOR BOARD 221MAF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 221MAF FROM TRAVELER T22/1602730 IAW DWG SRZ-25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.SDR FDEA202203100461Floorboard · delaminatedCOURIER AREA FLOOR BOARD 221AF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 221AF FROM TRAVELER T22/1602729 IAW DWG SRZ- 25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.SDR FDEA202203100460Floorboard · delaminatedCOURIER AREA FLOOR BOARD 221BF DELAMINATED. FABRICATED COURIER AREA FLOOR BOARD 221BF FROM TRAVELER T22/1602728 IAW DWG SRZ- 25-005. "MAJOR REPAIR" PART MARKED IAW GMM 07-0-1001.SDR FDEA202203100459Floorboard · delaminatedCOURIER AREA FLOOR BOARD 221MBF DELAMINATED. FABRICATED PANEL 221MBF COURIER AREA FLOOR BOARD FROM TRAVELER T22/1602791 IAW DWG SRZ-25-005 REV. R. "MAJOR REPAIR". PART MARKED IAW GMM 07-0-1001.SDR FDEA2020060531121Fitting · lack of lubeL1 DOOR WILL NOT ARM SLIDE. LUBED L1 DOOR GIRT BAR FITTINGS. L1 DOOR ARMS AND DISARMS NORMAL REF MM 25-66-10-2.SDR FDEA202004170756Valve · faultyRT ENG BLEED CAUTION ON TAKEOFF ROLL. REMOVED & REPLACED RIGHT ENGINE RFCC PER AMM 36-11-18-4. REMOVED & REPLACED RIGHT ENGINE HIGH STAGE PILOT VALVE PER AMM 36-11-08-4-2. PERFORMED OPS CHECK OF RIGHT ENGINE RFCC AND HIGH STAGE PILOT VALVE REF AMM 36-11-18-SDR FDEA2020041090727Skin · gougedRW INBOARD FLAP UPPER SURFACE HAS GOUGES REPAIRED RW INBOARD FLAP UPPER SURFACE GOUGES IAW B757 SRM: 51-40-02, 57-53-01-2A, 51-70-10, 51-20-05, AMM: 51-21-10/701, NDTM PT. 6 51-00-16, 51-00-19, NDTM PT. 4 51-00-05 & EA #F-5750-T0353383; F-5750-T0353383-P1 SDR FDEA2020041090726Skin · crackedLEFT WING I/B FIXED L/E SKIN BEHIND #5 SLAT CRACKED REMOVED DAMAGED LOWER SKIN AND CORE AND REPAIRED IAW B757 SRM 57-41-01 AND B757 SRM 51-70-08-0G. APPLIED FOIL TAPE TO INNER SKIN IAW B757 SRM 57-41-01-0I AND B757 AMM 51-21-04-7. RESTORED INNER SKIN FINISSDR FDEA2020040870709Stiffener · corrodedLAVATORY SERVICE DOOR STIFFENER IS CORRODED (119AL) REMOVED AND REPLACED LAVATORY SERVICE DOOR STIFFENER PER BAC DWG #141N8631 REV F AND B757 SRM 51- 40- 02 TOPCOATED AREA PER B757 SRM 51-20-01SDR FDEA202004060703Skin · dentedLEFT H.STAB UPPER SURFACE HAS NUMEROUS DENTS AUXILIARY SPAR TO FRONT SPAR. REPAIRED LEFT HAND STAB UPPER SURFACE DENTS IAW B757 SRM 55-10-01-1A NOTE I, 51-70- 10-0G, 51-70-10-2R, ALODINED PRIMED AND SEALED REPAIR IAW B757 MM 51-21-04, 51-21-10 AND B757 SRSDR FDEA2020040320658Strap · crackedAREA AFT OF THE AFT CARGO COMPARTMENT ST 1661 APPROX RBL 24 MISC MAIN CABIN FLOOR SUPPORT STRUCTURAL STRAP IS CRACKED REPAIRED STRAP IAW B757 SRM 53-00-51-2R PO:958485.5, PO:920167.4, PO:834933.1SDR FDEA201906281425Light · inoperativeEXTERIOR EMERGENCY LIGHT AFT OF L1 DOOR IS INOP. R&R LAMP REF MM 33_51_06_2_1. OPS CK GOOD.SDR FDEA201803140688Shear Tie · corrodedUPON REMOVAL OF DAMAGE OF RT SIDE TRANSITION PANEL, UNDERNEATH OF PANEL. FOUND CORROSION ON SHEAR TIE AT BS 1380 AND STR 26R. EVALUATED SHEAR TIE FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A, DETAIL V, FIG 101. REMOVED SHEAR TIE AT STA 1380 AND STR 26R IAW SRM 5SDR FDEA201803060607Floorbeam · crackedFWD CARGO BAY MAIN FLOORBEAM AT BS 580, LBL 45.5 IS CRACKED. REPAIRED IAW EA F-5310-T0338759.SDR FDEA201710203014Sequence Valve · failedON APPROACH, EXTENDED LANDING GEAR AND RECEIVED A GEAR DISAGREE EICAS. THE NOSE GEAR LIGHT WAS NOT ILLUMINATED. COMPLIED WITH QRH PROCEDURES AND USED THE ALTERNATE GEAR EXTEND SWITCH. UNEVENTFUL LANDING WITH GEAR DOORS LIGHT ILLUMINATED. REMOVED AND REPSDR FDEA201704251260Cover · delaminatedCAPTAIN'S ESCAPE ROPE COVER LATCH BROKEN & WILL NOT STAY IN PLACE. THE LATCH NOT BROKEN, BUT FOUND DELAMINATED. LAMINATED AND SECURED THE PANEL IAW AMM 25-51-00-4.SDR FDEA201703301027Lock · out of adjustMAIN CARGO DOOR LIGHT ILLUMINATED AT 5000 FT, 215 KB, DURING CLIMB OUT. QRH COMPLIED WITH. ADJUSTED FWD LOCK SWITCH IAW AMM 52-72-01-4. ACFT OK FOR SERVICE.SDR FDEA201607202557Power Supply · inoperativeLEFT EMERGENCY LIGHT ABOVE L1 DOOR INOPERATIVE. R & R EMERGENCY POWER SUPPLY ASSY IN REF WITH AMM 33-51-0702 AND 33-51-00/501. OPS CK'S GOOD AT THIS TIME.SDR FDEA201607202556Power Supply · inoperativeLEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE BY L1 DOOR. EMERGENCY POWER SUPPLY ASSY R & R UNDER WRI 33-50/2274. OPS CHECK IN REF WITH AMM 33-51-00/501.SDR FDEA201603010751Repair · debondedDISBOND TOP TE FIX FLAP, STATION 338, RT WING ON EXISTING REPAIR. REMOVED DISBONDED EXISTING REPAIR AND FABRICATED,PREPPED AREA AND HOT BONDED NEW REPAIR TO TOP TE FIX FLAP STA 338 RT WING IAW B757 SRM 51-70-10-2R REPAIR 4. TAP TEST PERFORMED, NO DELAM NOTEDSDR FDEA201502070467Pseu · failedRIGHT EMER DOOR EICAS ALERT CAME ON WITH, EMER DOORS OVERHEAD, DISCRETE LIGHT ON. R & R PSEU IAW AMM 32-09-04-4. ALL CHECKED GOOD. RT EMER DOOR IS NO LONGER DISPLAYED.SDR FDEA201408222289Battery Pack · unsecureON POST FLIGHT INSPECTION FOUND THAT L1 SLIDE EMER LIGHT & L1 DOOR OVERHEAD EMER EXIT LIGHTS ARE INOPERATIVE AMM. TROUBLE SHOT SYS, FOUND THAT BATTERY PACK WAS NOT SECURED TO THE M731 POWER SUPPLY CAUSING CONNECTION TO BE LOST. REATTACHED & POSITIVELY SECURESDR FDEA201403130498Skin · dentedDENT ON FUSELAGE SKIN AT BS 524, STRINGER 28R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED DENT IAW SRM 53-00-01, FIG. 201, REPAIR 15. MAJOR REPAIR.SDR FDEA201402170346Slat · damagedWING, NOTED DURING REPLACEMENT OF NR 7 SLAT INBD SEAL ON SNRM SEQ NR N01672, TWO EACH WRONG FASTENER RIVETS ARE INSTALLED & HOLES ARE FOUND ELONGATED. ACCOMPLISHED EA F-5750-T0304854, WINGS FLIGHT SURFACES NR 7 LE SLAT ELONGATED HOLES REPAIR.SDR FDEA201402130314Skin · scratchedFUSELAGE SKIN HAS SCRATCHES BS 1684 - 1694 BETWEEN STRINGER 13A - STRINGER 14A, LT. A SKIN REPAIR WAS ACCOMPLISHED AT STATION 1679 - 1700, STRINGERS 1 - 13A TO 15L, ON STAM WC 6000100458 & EA 757-5361-16-F4480.SDR FDEA201402030252Skin · damagedINCOMING FUSELAGE SKIN IMPACT STATION 1440 TO 1480, STRINGER 18R. A SKIN REPAIR STATION 1440 - 1480, STRINGER 17R - STRINGER 22R, WAS ACCOMPLISHED ON STAM WC 6000100363 & EA 757-5361-16-F4368, REV WITH FORM 8110-3 ATTACHED, IAW EA F-5330-T0304947. FUSELAGE PSDR FDEA201402030251Skin · damagedSCRIBE LINE FOUND AT STRINGER 20R LAP SEAM FROM BS 1439.625 TO BS 1459. SCRIBE LINE REPAIR AT LAP SEAM STRINGER 20R BETWEEN BS 1439.625 TO BS 1459 WAS ACCOMPLISHED ON STAM WC 6000100363 & EA 757-5361-F4368 REV. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY.SDR FDEA201401220176Skin · dentedLEFT UPPER LOBE EXTERNAL FUSELAGE SKIN CROWN AREA AT STATION 790, BETWEEN STRINGERS 2L & 2R HAS MULTIPLE DENTS. ACCOMPLISHED EA F-5330-T0304259 PT1, FUSELAGE PLATES & SKINS, SKIN SECTION 43. FUSELAGE SKIN DENT REPAIR NEAR STATION 780 & BETWEEN STRINGER 2L SDR FDEA201401210152Attach Angle · damagedNOTED VERTICAL TIP PANEL ATTACH ANGLES, BOTH LT & RT SIDES HAS NUMEROUS ELONGATED HOLES AT VERTICAL STAB TIP STRUCTURE. FOUND TO BE OUT OF LIMITS IAW DWG 172N3014 SHT 1 REV D. REMOVED ANGLES IAW SRM 51-40-02. FABRICATED NEW ANGLES IAW DWG 172N3014 & SRM 51SDR FDEA201401150105Tee Fitting · corrodedDURING REMOVAL CORROSION FOR NR N01645 FOUND T CHORD PN 148N3615 3 AT STATION 1885, STRINGER 27L TO STRINGER 27R CORRODED. REMOVED CORROSION ON T CHORD IAW SRM 51-10-02. ORIGINAL THICKNESS .125 INCHES, MATERIAL LOSS .016 INCHES, MATERIAL REMAINING .109 INCHESSDR FDEA201401030018Frame · dentedAFTER SKIN REPAIR, IT WAS NOTED A DENT ON FRAME FLANGE BS 223.5, 5 INCHES BELOW STRINGER 20R. REPAIRED IAW EA F-5330-T0304738. MAJOR REPAIR.SDR FDEA201401030019Skin · dentedDURING INSPECTION, A DENT WAS FOUND ON SKIN BS 377 BETWEEN STRINGER 23 - 24R. REPAIRED SKIN AREA IAW SRM 53-00-01 REP 16.SDR FDEA201312183010Skin · corrodedBULK CARGO BAY BILGE AREA AIRFONE SUPPORT DOUBLER & PLATE HAS LIGHT CORROSION INCLUDING DOME NUTS BS 1500 - 1520, STRINGERS 28 - 29L. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II. REPAIRED SKIN IAW SRM 53-00-01,
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