N930FD
Service difficulty reports · 176
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 = 'N930FD' 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 = 'N930FD' 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 FDEA201804030838Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT SPAR HAD TWO DENTS, HSS 127 - 133 AND FOUND TO BE OUT LIMITS. CUT OUT THE DAMAGE & APPLIED PERMANENT REPAIR IAW SRM 51-70-10-2R, REPAIR 3 & 4.SDR FDEA201804030837Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT SPAR HSS 138 - 143, ONE DENT FOUND OUT OF LIMITS. REMOVED DAMAGE, APPLIED PERMENANT REPAIR IAW SRM 51-70-10-2R, REPAIRS 3 & 4.SDR FDEA201804030836Skin · dentedLEFT HORIZONAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT STAB 144 - 150 HAD TWO DENTS FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-70-10-2R, REPAIR 3 & 4,SDR FDEA201804030839Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT SPAR HSS 124 - 130 DENTED OUT OF LIMITS. REMOVED DAMAGE, APPLIED A PERMENANT REPAIR IAW SRM 51-70-10-2R, REPAIRS 3 & 4.SDR FDEA201804020828Skin · crackedCRACK GOING OUT FROM SKIN AFT SIDE OF THE NR 1 SLAT FROM FASTENER. COMPLIED WITH EA F-5750-T0339279 P1. FABRICATED TWO REPAIR DOUBLERS, FILLERS & INSTALLED IAW SRM 57-43-01-2R, REPAIR 4.SDR FDEA201803240771Floorbeam · damagedMAIN CABIN FLOORBEAM FWD FLANGE BS 620, LBL 40 HOLE IS OBLONG. REPAIRED IAW EA F-5310-T0339088.SDR FDEA201803240770Floorbeam · damagedMAIN CABIN FLOORBEAM AT BS 580 FWD FLANGE, LBL 40 HOLE IS OBLONG. REPAIRED IAW EA F-5310-T0339086, P1.SDR FDEA201803240769Floorbeam · damagedMAIN CABIN FLOORBEAM BS 600 FLOOR PANEL MOUNT HOLE AT APPROX. LBL 40 IS OBLONG. REPAIRED IAW EA F-5310-T0339087.SDR FDEA201803210747Attach Fitting · crackedMAIN CABIN FLOORBEAM ATTACH FITTING AT BS 580, LBL 45 CRACKED IN AFT UPPER FLANGE. REPAIRED IAW EA F-5310-T0338866 P1.SDR FDEA201710243032Pressure Switch · failedRECEIVED A LT HYD SYS PRESSURE EICAS MESSAGE, ALONG WITH RUDDER RATIO EICAS MESSAGE ON EXTENDING FLAPS TO 1. LEFT HYDRAULIC QTY 1.0, LEFT HYDRAULIC PRESSURE 3100 PSI. R & R THE LT HYD SYS PRESSURE SWITCH IAW AMM 29-11-17-4. LEFT HYD PRESSURE SWITCH OPS ANDSDR FDEA201707031847Battery Pack · inoperativeFOUND DOOR 1R EMERGENCY LIGHTS NOT COMING ON DURING TEST. REMOVED AND REPLACED M730 POWER SUPPLY BATTERY PACK PER AMM 33-51-07-2, OPS CHECK NORMAL. A/C OK FOR SERVICE.SDR FDEA201602270697Skin · delaminatedRIGHT WING INBD FLAP, OTBD TE, UPPER SKIN HAS AREA OF DELAMINATION. HOT BONDED PERMANENT REPAIR ONTO RT WING I/B FLAP O/B TE UPPER SKIN IAW SRM 57-53-01-2R REPAIR 1 FIG 201 DETAIL 1 AND SRM 51-70-10-2R REPAIR 4. POST REPAIR TAP TESTED AREA IAW SRM 51-10-06-2SDR FDEA201602260695Shear Web · corrodedMAIN DECK SHEAR WEB BS 1684 - 1694, LBL 60 TO RBL 60, HAS CORRODED AREAS. REMOVED CORROSION, AND FOUND TO BE E OUT OF LIMITS IAW SRM 53-60-51-1A FIG 101 DETAIL III TABLE 102. FABRICATED DOUBLER REPAIR AND INSTALLED IAW SRM 53-60-51-2R FIG 201 DETAIL 1 ALTERNSDR FDEA201602260694Shear Plate · corrodedMAIN CARGO COMPARTMENT, FLOOR SHEAR PLATE CORRODED, BETWEEN BL 0 - LBL 24, BS 410 - 440. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 757-200, FABRICATED DOUBLER REPAIR AND INSTALLED IAW SRM. FOUND TO BE WITHIN LIMITS IAW SRM.SDR FDEA201602240681Skin · delaminatedRT INBD AFT FLAP HAS DELAMINATION AT OTBD AREA. EVALUATED AREA TO BE .025" DEPTH X2.5 ' LENGHT AND FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01-1A FIG 101. ACCOMPLISHED PERMANENT REPAIR TO RT I/B AFT. FLAP UPPER SKIN IAW SRM 57-53-01-2R FIG 201,TABLE II AND SDR FDEA201503271094Light · inoperativeLEFT FRONT ENTRY DOOR SLIDE LIGHT INOPERATIVE. REPLACED BULB GE 767 IAW MM 33-51-06-2-1. LIGHT OPERATIONS CHECKED NORMAL, OK FOR SVC.SDR FDEA201412194151Stowage Box · failedAT BLOCK IN POST FLIGHT CHECK FOUND CAPTAIN`S O2 MASK WOULD NOT TEST. R & R CAPTAIN`S O2 STORAGE BOX IAW MM 35-11-51-4-99. OPERATIONS & LEAKS CHECKED GOOD.SDR FDEA201412094088Light · inoperativeEMERGENCY LIGHTS UNARMED ANNUNCIATOR LT HALF UNLIT. REMOVED & RE LAMPED EMER LIGHT UNARMED ANNUNCIATOR LIGHT. OPERATIONS CHECKED GOOD IAW MM 33-13-00-2. ACFT OK TO CONTINUE.SDR FDEA201411193808Slide · malfunctionedUPON ARRIVAL, L1 DOOR WAS OPENED WITH THE SLIDE ARMED. SLIDE CAME OUT BUT DID NOT DEPLOY. MEL 19 NOV 14 13:59 RELEASED FOR SERVICE IAW MEL 52-11-01-A CATEGORY B EXPIRATION 22 NOV 14 MEL 52-11-01-A. L1 DOOR SLIDE MISSING, IDENTIFY INOPERATIVE OR MISSING. RSDR FDEA201406101379Window · failedLEVEL AT 390, FIRST OFFICER`S WINDOWS SHATTERED. REPLACED WINDOW.SDR FDEA201401250195Slide · unsecureLEFT ENTRY DOOR SLIDE PARTIALLY UNSTOWED. COMPLIED WITH ESCAPE SYS INSPECTION & CHECKED IAW MM 25-66-01-6. L1 DOOR OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA201306111249Lamp · inoperativeR1 SLIDE LIGHT WILL NOT ILLUMINATE WHEN THE DOOR IS ARMED. REPLACED LAMPS IAW STD MAINT PRACTICES, OPS CHECKED OK.SDR FDEA201302150354Cover · detachedL-1 DOOR SLIDE COVER, BOTTOM SEAL IS DETACHED FROM COVER. REINSTALLED L1 ESCAPE SLIDE COVER IAW AMM CHPT 25-66-00-2. SLIDE COVER LOCKED AND SECURED, ACFT OK FOR SERVICE. FINAL CLOSED.SDR FDEA201202010422Shear Tie · crackedUPON REMOVAL OF WING TO BODY SUPPORT, FOUND SHEAR TIE CRACKED AT STA 1300, STR 20L. REMOVED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE IAW DWG NR 140N2002-1059 AND SRM 51-30-01 AND 51-40-5. INSTALLED SHEAR TIE IAW SRM 51-40-02.SDR FDEA201110074363Lens · brokenLENS CAP ASSY ON EMERGENCY LIGHT UNARMED ANNUNCIATOR BROKEN. R & R EMERGENCY LIGHT UNARMED ANNUNCIATOR LENS CAP ASSY, DIODE/FUSE CARD AND DRAWER ASSY. OPS CHECKED GOOD WITH EMERGENCY LIGHTS ARMED/UNARMED. AMM 33-16-02-2.SDR FDEA201011184422Connector · damagedPASSING 17000FT, FLAPS RETRACTED, CLEAN CONFIGURATION, RECEIVED L/E SLAT ASYM EICAS ALONG WITH T/E CAUTION LIGHT. AT DESTINATION, FLAPS COULD NOT EXTEND WITH HYD EXTENDED FLAPS IAW QRH ELE WITH ALTN FLAP SWITCH. PERFORMED BITE ON ALL 3 FSEU'S. NO CURRENT FSDR FDEA201010023887Frame · damagedLOWER LOBE- AVIONICS COMPT FWD OF NWW- FRAME 231.25 HAS DOOR LOCK PIN IMPACT DAMAGE AT BL "0", ALSO DOOR LOCK FITTING ATTACHED TO FRAME DAMAGED. REPAIRED FRAME 231.25 BL "0" AT AVIONCS COMPT FWD OF NWW IAW EA F-5310-141195, FUSELAGE STA 231.25, LOWER LOBE SDR FDEA201009303822Door Frame · gougedNR 1 CARGO DOOR LOWER FRAME HAS 3 GOUGES BLENDED GOUGES ON NR 1 CARGO DOOR LOWER FRAME AND FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02 FIG 101 DETAIL VII. REMOVED AND REPLACED FRAME IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201009233690Skin · misaligned2 EA OVERSIZED FASTNER HOLES ON OUTER LOWER EXTERIOR FUSELAGE SKIN AT STA 501, WL 220, LBL 70. DWG REQUIREMENT- .159 TO .165 DIAM. ACTUAL SIZE .191 2EA FASTENER HOLES ON OUTER LOWER EXTERIOR FUSELAGE SKIN PN 143N8161-2 AT STA 501, WL 220, LBL 70 WERE OVERSIZSDR FDEA201009233675Seat Track · misalignedINCOMING FASTNER HOLES IN FLOORBEAM UPPER FLANGE INTERFERS WITH 657N3332-2 SEAT TRACK INSTALLATION AT STA 620, 640, 660. RBL 58.22 AT STA 620, 640, AND 660 RBL 58.22. FLOORBEAM REPAIR WAS ACCOMPLISHED ON MAE EA 757-5335-16-F2773 REV- DATED JUL 9, 2010. MAJOSDR FDEA201009233671Stringer · damagedELONGATED HOLE FOUND IN INCOMING STRINGER AT STA 437, S-22L AT STA 437, S-22L STRINGER REPAIR WAS ACCOMPLISHED ON MAE EA 757-5332-16-F2732, REV- DATED JUN 15, 2010. MAJOR REPAIR.SDR FDEA201009233670Floorbeam · misalignedSHORT EDGE MARGIN CONDITIONS FOUND IN 146N5044-4 FLOORBEAM UPPER FLANGE AT STA 1280, RBL 24.75 AND RBL 45.50 AT STA 1280, RBL 24.75 AND 45.5 FLOORBEAM UPPER FLANGE REPAIR WAS ACCOMPLISHED ON MAE EA 757-5365-16-F2762, REV- DATED JUN 24, 2010. MAJOR REPAIR.SDR FDEA201009233669Fitting · misalignedPOTENTIAL SHORT EDGE MARGIN CONDITIONS IN 657N3161-11 FITTING DUE TO INCOMING FASTNER HOLE LOCATIONS AT STA 1640 BETWEEN S-17L TO S-18L AT STA 1640 BETWEEN S17L TO S18L FRAME REPAIR WAS ACCOMPLISHED ON MAE EA 757-3562-16-F2757 REV- DATED JUN 22, 2010. THIS NSDR FDEA201009233668Seat Track · damaged1EA INCOMING FASTNER HOLE INTERFERS WITH INSTALLATION OF 657N3329-2 SEAT TRACK AT STA 640, LBL 58.22 AT STA 640, LBL 58.22 FLOORBEAM FLANGE REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION ON MAE EA 757-5335-16-F2819 REV- DATED AUG 6,SDR FDEA201009233667Floorbeam · damagedDISCREPANT FASTNER HOLE IN FLOORBEAM AT STA 460, LBL 68 AT STA 460, LBL 68. FLOORBEAM REPAIR WAS ACCOMPLISHED ON MAE EA 757-5335-16-F2740 REV- DATED JUN 17, 2010. MAJOR REPAIR.SDR FDEA201009233659Skin · crackedNR7 SLAT UPPER SURFACE HAS 2 EA CRACKS FOUND NR 7 SLAT TO BE OUT OF LIMITS IAW SRM 57-43-01 FIG 101. NR 7 SLAT REMOVED AND REPLACED ON WO 00047415, N01466. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201009213604Skin · damagedEXTERIOR SKIN UNDER ELT STA 1500-1520 SKIN IS DISTORTED COMPLIED WITH EA F-5330-142238 FUSELAGE PLATES AND SKIN-BS 1500 TO STA 1520 BETWEEN S-1 AND S-2L SKIN REPAIR. MAJOR REPAIRSDR FDEA201009173518Skin · dentedNR 9 SLAT L/E UPPER SURFACE HAS DENT REPAIRED NR 9 L/E SLAT UPPER SURFACE AT STA 594.50 APPROX 5" FWD OF T/E IAW SRM 57-43-02. FINAL REPAIR DIMENSION WAS 4" IN DIAM. CATEGORY "A" MAJOR REPAIR.SDR FDEA201009103338Gate · corrodedR4 DOOR LOWER GATE, LOWER EDGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG. 101 XII. REMOVED AND REPLACED R4 LOWER GATE ASSEMBLY IAW AMM 52-11-38-4. ADJUSTED R4 DOOR IAW AMM 52-11-00-5.SDR FDEA201009093328Skin · dentedREWORK- DENT WAS FOUND ON FIRST EVALUATION TO BE OUT LIMITS, WAS RE-EVALUATED AND BLOCK 26 "CORRECTIVE ACTION" STATED TO BE FOUND WITHIN LIMITS. SECOND EVALUATION DID NOT ADDRESS FIRST EVALUATION OUT OF LIMITS CONDITION "DENT IS WITHIN .5" PROXIMITY OF SSDR FDEA201009093327Gate · gougedR 1 DOOR LOWER GATE , FWD & AFT CORNERS HAVE GOUGES. R 1 DOOR LOWER GATE , FWD & AFT CORNERS HAVE GOUGES REMOVED GOUGES ON R1 DOOR LOWER GATE AND FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG 101 DETAIL XII. REPLACEMENT OF LOWER GATE ACCOMPLISHED ON NR N0172SDR FDEA201009093326Gate · corrodedR1 DOOR LOWER GATE, LOWER EDGE HAS CORROSION. REMOVED CORROSION FROM R1 DOOR LOWER GATE AND FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DETAIL XII. R & R LOWER GATE ON NR N01728 IAW AMM 52-11-38. CLASSIFIED MAJOR REPAIR.SDR FDEA201009033267Gate · corrodedL1 DOOR LOWER GATE LOWER EDGE HAS CORROSION. REMOVED L-1 DOOR LOWER GATE FOUND OUT OF LIMITS IAW SRM 51-10-02. INSTALLED L-1 LOWER GATE IAW AMM 52-11-38. PERFORMED OPERATIONAL AND ADJUSTMENT CHECKS FOUND SATISFATORY IAW AMM 52-11-00 IN C/W N00134.SDR FDEA201009013238Skin · dentedNR 7 SLAT HAS SEVERAL DENTS UPPER SURFACE. REPAIRED NR 7 SLAT IAW SRM 57-43-02, SLAT NR 7 PN 114N4005-178A, SN A2-0348, STA 341.50, BONDED 4" DOUBLER OVER DENT NR 1 DENT NR 2 IS A=.655, Y=.006, A/Y=109.1, DENT NR 2 TO BE IN LIMITS IAW SRM 57-43-02, FIG 101, DESDR FDEA201009013236Frame · gougedMAIN DECK FRAME BS 1640, BETWEEN S- 5L & S-6L GOUGED AT BS 1640 FRAME, S5-6L.SDR FDEA201009013234Skin · crackedDENT AT BS 223.5 ABOVE S23L , EXT FUSELAGE SKIN WAS DETERMINED " OUT OF LIMITS " AND "REWORKED TO ORIGINAL CONTOUR" BY PREVIOUS OPERATOR, SRM REQUIRES A REPAIR BE ACCOMPLISHED EVALUATED DENT. CRACK INDICATIONS NOTED PER NDTM, PT.6, 51-00-19. CRACK: 1.SDR FDEA201009013232Floor Support · corrodedMAIN DECK FLOOR LEFT SHEAR WEB INBD SUPPORT ANGLE, BS 755, HAS CORROSION. REMOVED CORROSION LT SHEAR WEB SUPPORT ANGLE, BS 755-900, IAW SRM 51-10-02. CHECKED LIMITS; ORIG MATL .071", LOSS: .008", REMAINING: .063". FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13SDR FDEA201008303197Skin · dentedNR 6 SLAT LEADING EDGE HAS CREASE DENT UPPER SURFACE WS 150.5 EVALUATED DENT AND FOUND TO BE OUT OF LIMITS PER SRM 57-43-02, FIG.101, AND NOTE "K"; A=1.11, Y=.066", A/Y=16.83. REPAIRED NR 6 L/E SLAT, UPPER SURFACE, PER SRM 57-43-02, BY BONDING A 4" DOUBLER SDR FDEA201008303195Wedge · dentedDENT ON NR 3 L/E SLAT UPPER SURFACE T/E WEDGE AT SLAT OSS 503.75 EVALUATED DENT ON NR 3 SLAT T/E WEDGE OSS 503.75 A=1.115 Y=.026 A/Y RATIO 42.8 FOUND TO BE OUT OF LIMITS DUE TO DELAMINATION IAW SRM 57-43-02 FIG 101 NOTE "K". REPAIRED SLAT IAW SRM 57-43-02 BONDSDR FDEA201008303194Skin · dentedRT WING INBD FLAP DENTED AT APPROX WS 369.5 LOWER SURFACE EVALUATED DENT ON RT WING INBD FLAP LOWER SURFACE WS 369.5 A=1.187 Y=.062 A/Y RATIO 19.1 FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01, FIG 101, DETAIL VII. REPAIRED FLAP IAW SRM 57-53-01. CLASSIFIED CAT
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