N993FD
Service difficulty reports · 134
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 = 'N993FD' 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 = 'N993FD' 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 FDEA201406071341Wedge · damagedNUMBER 2 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 2 SLAT ASSEMBLY IAW-AMM-27-81-02 ADJUSTMENT TEST GOOD IAW AMM- 27-81-02-4, CAT A MAJOR REPAIR.SDR FDEA201406071340Wedge · damagedNUMBER 1 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 1 SLAT ASSEMBLY IAW-AMM-27-81-02, ADJUSTMENT TEST GOOD IAW-AMM-27-81-02-4, CAT A MAJOR REPAIR.SDR FDEA201406071339Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 113 INCHES FROM OTBD END 2 INCHES FROM AFT EDGE. REPAIRED RT OTBD AFT FLAP WEDGE UPPER SURFACE IAW-SRM-57-53-01 & SRM-51-70-04 CAT A MAJOR REPAIR.SDR FDEA201406071338Wedge · damagedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE PUNCTURED 67 INCHES FROM INBD END 4 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04 CAT A MAJOR REPAIR.SDR FDEA201406071337Wedge · damagedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE PUNCTURED 66 INCHES FROM INBD END 10 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM- 51-70-04, CAT A MAJOR REPAIR.SDR FDEA201406071336Wedge · damagedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE PUNCTURED 18 INCHES FROM INBD END, 8 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04 CAT A MAJOR REPAIR.SDR FDEA201406071335Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 22 INCHES FROM INBD END, 111/2 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04, CAT A MAJOR REPAIR.SDR FDEA201406071334Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 57 INCHES FROM INBD END, 5 1/2 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04, CAT A MAJOR REPAIR.SDR FDEA201406071333Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATION DENT 32 INCHES FROM OTBD END, 5 INCHES FROM AFT EDGE. REPAIRED RT OTBD AFT FLAP WEDGE UPPER SURFACE IAW SRM 57-53-91 & SRM 51-70-04.SDR FDEA201406071332Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 36 INCHES FROM INBD END, 7 INCHES FROM AFT EDGE. BONDED & REPAIRED, RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04, CAT A MAJOR REPAIR.SDR FDEA201406071331Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 53 INCHES FROM INBD END, 91/2 INCHES FROM AFT EDGE. BONDED & REPAIRED, RT OTBD AFT FLAP IAW SRM-57-53-01 & 51-70-04, CAT A MAJOR REPAIR.SDR FDEA201406071330Wedge · delaminatedRIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATION DENT 77 INCHES FROM OTBD END, 2 INCHES FROM AFT EDGE. REPAIRED RT OTBD AFT FLAP WEDGE UPPER SURFACE IAW SRM 57-53-01 & SRM 51-70-04.SDR FDEA201406071329Skin · damagedLEFT WING OTBD FLAP AFT FLAP UPPER SURFACES HAS SEVERAL AREAS WITH HAIL STRIKES. BONDED & REPAIRED LT WING OTBD FLAP, AFT FLAP, IAW SRM-57-53-01 & SRM-51-70- 04, APPROX .5 INCHES IN DIAMETER. REMOVED 4 INCHES. REPAIRED THREE AREAS, 1ST LOCATED AT 13.5 INCHESDR FDEA201406071328Wedge · delaminatedRT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 59 INCHES FROM OTBD END, 71/2 FROM AFT EDGE. REPAIRED RT AFT FLAP WEDGE UPPER SURFACE IAW SRM 757 51-70-04.SDR FDEA201305080942Light · corrodedTHE L1 ENTRY DOOR ESCAPE SLIDE LIGHT INOP. T/S ESCAPE SLIDE LITE,TESTED BATTERY PACK IAW MM 33-51-07-2-2, BATTERY PACK OP'S NORMAL, REMOVED LAMP AND REMOVED CORROSION FROM RECEPTICLE, RE INSTALLED LAMP, TESTED EMERGENCY LIGHTS IAW MM 33-51-06-2-1. ESCAPE LIGSDR FDEA201304190835Wire · unknownCOCKPIT EMERGENCY LIGHT INOPERATIVE. FOUND NO WIRE IN PIN 12 OF D68 ON M731, WIRE W3532-0160-22 IS CAPPED AND STOWED AT D68 AND IS THE WIRE CALLED OUT IN WDM 33-51-12. WIRING LIST FOR D68 SHOWS WIRE 0502- 22 CONNECTED TO PIN 12 FOR THIS AIRCRAFT. APPEARS THSDR FDEA201303160587Valve · malfunctionedDURING CRUISE FL400, LT ENGINE BEGAN TO SURGE WITH EPR, N1, EGT, N2, FOLLOWING. QRH PROCEDURES STARTED. TRIED TO RETURN THRUST LEVER TO NEAR NORMAL. SURGING BEGAN AGAIN. REDUCED THRUST TO IDLE. TURNED BLEED OFF. ENGINE RESPONDED. TURNED ENGINE BLEED ON AS LSDR FDEA201302100316Control Panel · malfunctionedON ROLLOUT RECEIVED "MAIN CARGO FIRE" WARNING LASTED MAYBE 2-4 SEC, THEN WENT OUT. PASSENGER OXYGEN WENT ON. REPLACED MAIN DECK SMOKE CONROL PANEL IAW AMM P TO F26-16-30. MAIN DECK CARGO DETECTION. OPS CHECKS NORMAL IAW P TO F AMM 26-16-30, P 501.
ACFT RSDR FDEA201212114282Shear Tie · crackedAFT CARGO BS 1300 FRAME HAS CRACKED SHEAR TIE BETWEEN STR 20L AND STR 21L. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW AND INSTALLED IAW SRM 51-40-02, 51-40-05, 51-70-11 AND DWG 140N2002 REV EU.SDR FDEA201212104274Angle · crackedNR 2 PYLON, STA 102.1 INBD SIDE ANGLE CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-40-02 AND INSTALLED NEW ANGLE IAW SRM 51-40-02 AND DWG 311N3510 REV C.SDR FDEA201207272716Proximity Switch · malfunctionedON APPROACH, RECEIVED A L/E SLAT ASYM ALERT. ACFT DID NOT HAVE CONTROL PROBLEMS. UNABLE TO EXTEND FLAPS BEYOND 0 DEGREE AND 1 DEGREE, HYDRAULICALLY. USED ALTERNATE FLAPS FOR LANDING. R & R LOSS SENSING SWITCH FOR INBOARD LE SLATS IAW AMM 27-81-41-4, THRUSDR FDEA201106262429Ring · dislodgedL1 DOOR HAS STRAP AND D-RING HANGING DOWN OUT OF DOOR PACKAGE. RELEASED FOR SERVICE IAW MEL: 52-11-01-A CATEGORY: B EXPIRATION: 29JUN11 "MEL 52-11-01-A: L1 DOOR SLIDE- INOP (IDENTIFY INOP OR MISSING)." FOUND D-RING TO INTERFEAR WITH ARMING GIRT BAR, REPOSTIOSDR FDEA201105201905Slide · malfunctionedL1 CREW ENTRY DOOR SLIDE LIGHT WAS DIFFICULT TO ARM. OPS CHECKED L1 DOOR SLIDE ESCAPE SYSTEM REF MM 25-66-00-5-0. OPS CHECK GOOD, ACFT OK FOR SERVICE.SDR FDEA201101310427Stringer · corrodedREWORK OF NR N00451: FWD CARGO PIT STA 770, S-27L, WL 138 CORRODED REQUIRES REWORK DUE TO INCORRECT SRM REF USED REWORKED REPAIR SPLICE AT STA 770 S-27L . INSTALLED SPLICES IAW SRM 53-00-03 REPAIR 3 CAT "A" MAJOR REPAIR.SDR FDEA201101310428Skin · misrepairedPREVIOUS OPERATOR INSTALLED REPAIR EVALUATED IAW INCORRECT SRM REF. COMPLIED WITH EA F-5330-146251. FUSELAGE PLATES AND SKINS EO F-5100-7-5001 PART 1-EXISTING REPAIR TRACKING (DTA REQUIRED). MAJOR REPAIR.SDR FDEA201101310425Stringer · corrodedCORROSION ON S-26L BETWEEN STA 760-780 INSIDE FWD CARGO COMPARTMENT REQUIRES REWORK DUE TO INCORRECT SRM REF USED. REWORKED REPAIR SPICE AT STA 760-780 ON S-26L. RECEIVED NEW FILLER AND SPLICES ON T11/867864 AND T11/868216. INSTALLED NEW FILLER AND SPLICES ISDR FDEA201101250349Skin · dentedDENT ON FUSELAGE SKIN STA 580-600 BETWEEN S-27L TO S-28L. DENT AT STA 580-600 BETWEEN S-27L TO S28L FOUND OUT OF LIMITS DUE TO PROXIMITY TO FRAME IAW SRM 53-00-01, FIG 101 DETAIL III. REPAIRED SKIN IAW SRM 53-00-01, PG 201, FIG 201, REPAIR 16. CATEGORY "B" SDR FDEA201101250348Skin · dentedDENT ON FUSELAGE SKIN, STA 333.45 BETWEEN S-21L TO S-22L REQUIRES REWORK DUE TO INCORRECT SRM REF USED. DENT ON FUSELAGE SKIN STA 333.45 BETWEEN S-21L TO S-22L FOUND OUT OF LIMITS DUE TO PROXIMITY TO FRAME IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED SKSDR FDEA201101250350Skin · dentedREWORK OF NR N00182: EXTERNAL FUSELAGE SKIN FOUND DENT AT STA 1120-1139, S-8R DENT AT STA 1120-1139, S-8R FOUND OUT OF LIMITS DUE TO PROXIMITY TO STRINGER IAW SRM 53-00-01, FIG 101 DETAIL II. REPAIRED AREA IAW SRM 53-00-01, FIG 201, PG 204, TABLE 1 REPAIR SDR FDEA201101060064Bulkhead · gougedNR 2 PYLON AFT BULKHEAD GOUGED INBD AND OTBD LOWER CORNER. COMPLIED WITH EA F-5450-141204- NACELLES/ PYLONS -(AD 2003-18-05), ENGINE STRUT AFT BULK HEAD LOWER CORNERS CHAFED USING REPAIR PARTS FABRICATED ON TRAVLERS. T10/852810, T10/852831, T10/852832. THIS SDR FDEA201101050013Spar · gougedBETWEEN AFT SPAR AND RUDDER RIB STA 97.354 LT SIDE HAS 2 GOUGES. REPAIRED DAMAGE IAW EA F-5530-143212. STABILIZER-VERTICAL-ELONGATED HOLES IN TRAILING RIB. MAJOR REPAIR.SDR FDEA201101030003Skin · gougedRT WING INBD MAIN FLAP OTBD END AREA T/E LOWER SIDE HAS CHAFED AREA. REMOVED GOUGE ON RT WING I/B MAIN FLAP O/B END AND FOUND OUT OF LIMITS IAW SRM 57- 53-01 FIG 101 DETAIL V. REPAIRED FLAP IAW SRM 57-53-01 REPAIR 2. EA F-5750-146241. MAJOR REPAIRSDR FDEA201012294762Skin · damagedSCRIBE LINE FOUND AT STA 664.438-668.813 S26L. DURING LAP SEAM INSP, REPAIRED DAMAGE TO SKIN STA 664-668 S-26L PER EA F-5330-142243 FUSELAGE -PLATES AND SKIN - AD2007-19-07/EO F-5330-7-5000-SCRIBE LINE FINDINGS. MAJOR REPAIRSDR FDEA201012094627Skin · gougedGOUGE ON RT FUSELAGE SKIN NEAR R-2 DOOR UPPER FWD CORNER, STA 686,STR 7R. REPAIR ACCOMPLISHED IAW EA 757-5331-16-F2978 REF FAA FORM 8110-3, DATED NOV 22, 2010. (FIRST STAGE APPROVAL DTA PENDING) REF EA F-5330-1432220. THIS NR IS FOR TRACKING PURPOSES ONLY. SDR FDEA201012074605Floor Support · corrodedMAIN CARGO COMPARTMENT FLOOR SUPPORT HAS CORROSION BS 324 TO BS 350, RBL 40 TOP SIDE. REMOVED CORROSION IAW SRM 51-40-02. ORIG MAT THICKNESS .100 MAT LOSS .031 MAT REMAINING .069 FOUND AREA OUT OF LIMITS IAW SRM 53-00-51, PAG 103, DETAIL III, FIG 101. R & SDR FDEA201011224461Skin · dentedEXTERNAL FUSELAGE SKIN, FOUND DENTED AT BS 1120-1139.819, STRINGER 8R. FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO STR IAW SRM 53-00-01, FIG 101, DETAIL. REPAIRED DAMAGED AREA IAW SRM 53-00-01, FIG 201, REPAIR 2. CLASSIFIED CATEGORY "B" MAJOR REPAIR WITHSDR FDEA201011174407Gate · corrodedL-4 DOOR UPPER GATE HAS CORROSION. R & R L-4 PASSENGER ENTRY DOOR UPPER GATE IAW MM 52-11-38-4 AND SRM 51-10-02, FIG 101. PERFORMED ADJUSTMENT CHECK IAW MM 52-11-00-5. MAJOR REPAIR.SDR FDEA201011164399Skin · dentedDENTS ON FUSELAGE SKIN STA 580-600 BETWEEN STR 27L-28L EVLAUATED DENT AT STA 580-600 BETWEEN S-27L TO S28L AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101 DETAIL III, DUE TO DENT BEING LESS THAN .5 FROM FRAME. REPAIRED DAMAGED AREA IAW SRM 53-00-01, FSDR FDEA201011154379Seat Track · misalignedMAIN CARGO COMPARTMENT SEAT TRACK TOP HAS DOUBLE HOLES. BS 740 TO 760 RBL 45.50. FOUND DOUBLE HOLES AT FLANGE OUT OF LIMITS IAW SRM 53-00-52, DETAIL "G", FIG 101 PG 101. R & R SEAT TRACK IAW SRM 51-40-02 AND 51-20-05 AT BS 640- 780, RBL 45.50. MAJOR REPAIRSDR FDEA201011154378Frame · crackedMCD UPPER LOBE- FRAME AT STA 1520, S3L CRACKED. REMOVED DAMAGED AREA IAW SRM 51-10-02. FABRICATED NEW FRAME SECTION ON TRAV T10/854913, CHANNEL NR1 (2EA) TRAV T10/854912 & CHANNEL NR2 (2EA) TRAV T10/854911. LOC & DRILLED IAW SRM 53-00-07. TREATED & PRIMED SDR FDEA201011114319Skin · damagedACFT SKIN STA, 686 DAMAGED AT STRINGER 7R AT STA 686 STR 7R A MAJOR REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F MOD ON STAM W/O 11850045JUPR07 AND STAM EA 757-5331-16-2978, REV NEW DATED NOV 3, 2010. THIS NR IS FOR TRACKING PUPOSES ONLY ANSDR FDEA201011114318Frame · crackedMCD UPPER FRAME AT STA 1560 CRACKED AT STR 2R. REMOVED DAMAGED FRAME SECTION IAW SRM 53-00-07, REPAIR 1 FABRICATED NEW FRAME SECTION AND REPAIR PARTS ON TRAVELERS T10/854916, T10/854914 AND T10/854915. LOCATED AND DRILLED IAW SRM 53-0007 COLD WORK HOLES IAW SDR FDEA201011074269Seat Track · gougedMAIN CARGO COMPT. SEAT TRACK HAS CHAFFED MARKS, GOUGES, AND NICKS STA 640-780 RBL 24.75 REMOVED DAMAGE ON SEAT TRACK STA 640-780 RBL 24.75 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I. ORIG MATERAIL .265 REMOVED .025. MAX MATERIAL LOSS SDR FDEA201011054262Crease Beam · corrodedMAIN CARGO COMPARMENT CREASE BEAM HAS CORROSION RBL 62, BS 1260-1290. BLENDED CORROSION IAW SRM 51-10-02, CHECKED LIMITS ORIG MAT .070 MAT. REMAINING .059 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, PG 105, FIG 101, DET. VIII, R & R CREASE BEAM FROM STA 11SDR FDEA201011014204Skin · damagedNR1 PYLON LT SIDE SKIN 1 EA AND RT SIDE SKIN HAS 2 EA ELONGATED HOLES AT AFT BULKHEAD. COMPLIED WITH STAM EA 757-5450-16 F2907 REV - ELONGATED FASTENER HOLE FOUND IN THE RT AND LT SKIN OF NR1 PYLON COMMON TO BULKHEAD AT PP STA 201.5. EA F-5450-14227 NACELLESDR FDEA201010294195Structure · corrodedL-2 DOOR INNER CHORD HAS SURFACE CORROSION BET BSTA 700-720 LBL 64. BLENDED AREA & REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS, MATERIAL THICKNESS .080", MAT LOST .010" MATERIAL REMAINING .070" WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, PAG 106, DSDR FDEA201010284187Floorbeam · dentedMAIN CARGO COMPARTMENT FLOORBEAM HAS DENT BS 310.5. DENTS ON FLOOR BEAM STA 310.5 NOT PERMITTED IAW SRM 53-00-51 FIG 101. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02. CLASSIFIED CAT "A" MAJOR REPAIRSDR FDEA201010264173Structure · damagedNR1 PYLON 1EA CODE L HOLE INCOMING DIA. .312, EO F-5450-7-5010 P5 CALLS FOR .2651-.2661 COMPLIED WITH EA F-5450-141205. NACELLES/PYLON-NR 1-INCOMING OVERSIZED HOLES. CLASSIFED CATEGORY "A" MAJOR REPAIR.SDR FDEA201010244158Bulkhead · gougedNR 2 PYLON AFT BULKHEAD GOUGED INBD AND OTBD LOWER CORNERS. MACHINED DAMAGED AREAS, FABRICATED & INSTALLED REPAIR FILLERS AND GUSSETS IAW EA F-5450-141204 AND TRAVLERS T10/852810, T10/852831, T10/852832. MAJOR REPAIR.SDR FDEA201010234153Skin · dentedDENT ON FUSELAGE SKIN STA 33.45 BETWEEN S-21L TO S-22L. FOUND OUT TO BE OUT OF LIMIT IAW SRM 53-00-01, PG 101. DETAIL IV HFEC ON CUT- OUT & INITIAL FUSELAGE HOLES IAW NTM 51-00-19PT 6, NO CRACK NOTED. FABRICATED DOUBLER AND FILLER IAW SRM 53-00-01 PG 201, TAB
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