N936FD
Service difficulty reports · 229
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 = 'N936FD' 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 = 'N936FD' 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 FDEA202312141942Coupling · damagedAT CRUIRE AT FL 340 HAD A LT ENGINE FIRE (L ENG FIRE) AND OVERHEAT (L ENG OVERHEAT) INDICTION ON EICAS , LT FIRE HANDLE AND LEFT CONTOL LEVER. NO UNUSUAL LT ENG INDICATIONS OR VIBRARATIONS OBSERVED., LT EGT REMAINED WITHIN LIMITS ENTIRE TIME. FOLLOWED QRSDR FDEA202311161857Flex Line · leakingIN SHORT FINAL AFTER FULLY CONFIGURED, L HYD SYS PRESS EICAS CAME ON. LANDED WITH ROLL TO RIGHT, NO NOSE WHEEL STEERING. FACT 15NOV23 23:59 MEM U AMM: 20-10-10-4 AMM: 29-11-00-2 FIM: 29-11 F/T 808 AMM: 32-21-09-4 DURING INSPECTION AND CHECK FOUND SDR FDEA202309141597Skin · damagedDURING DVI INSPECTION OF L/E SKIN REPAIR ON #3 SLAT ON HECO CARD 9019, FOUND 2 BLIND FASTENERS THAT WERE LOOSE AND LOCKING PINS WERE NOT FLUSH WITH THE FASTENER HEAD. REMOVED AND REPLACED 2 EACH FASTENERS PER FEDEX EA# F-2780-T0350154 A P3 TITLE: FLIGHT COSDR FDEA202309131593Skin · corroded#1 PYLON PANEL 433HR HAS CORROSION ON AFT SURFACE OF THE PANEL FABRICATED NEW PANEL PER BAC DWG 311N5049 REV C AND FEDEX EA # F-5430-T0376029 TITLE: NACELLS/PYLONS - SKIN/PLATES/PANELS - #1 PYLON, STRUT ACCESS PANEL ASSY (443HR), FABRICATIONSDR FDEA202309131592Compressor · loose#1 ENG FAN CASE AREA PROTECTIVE PLASTIC COVER FOR KEVLAR SEPERATING FROM COMPRESSOR CASING AT FWD EDGE SEVERAL PLACES REPAIRED #1 ENGINE LP COMPRESSOR CASE TEFLON SLEEVE WITH PATCH IAW B757 AMM: 72-34- 10-8-4SDR FDEA202309131591Compressor · torn#2 ENGINE LP COMPRESSOR CASE KEVLAR WRAPPING FWD EDGE, PROTECTIVE PLASTIC COVER TORN AT 4 O'CLOCK POSITION. REPAIRED #2 ENGINE LP COMPRESSOR CASE TEFLON SLEEVE WITH PATCH IAW B757 AMM 72-34- 10-8-4SDR FDEA202309131590Compressor · loose#2 ENG LP COMPRESSOR CASE KEVLAR WRAPPING PROTECTIVE PLASTIC COVER, SEVERAL REPAIRS PATCHTAPE PEELING OFF. REPAIRED #2 ENGINE LP COMPRESSOR CASE TEFLON SLEEVE WIHT PATCH IAW B757 AMM 72-34- 10-8-4SDR FDEA202309111572Attach Angle · crackedLOWER FRAME ATTACH CLIP IS CRACKED IN LH MLG WHEEL WELL, ON AFT SIDE OF FRAME @ APPROX. STA 1064 LBL 30 REMOVED AND REPLACED CRACKED CLIP WITH NEW CLIP P/N 654N0243-13 PER BAC DWG 149N7550 REV HSDR FDEA202309101570Floor Support · crackedAFT PIT CARGO COMPARTMENT FLOOR STRINGER HAS A CRACK ON STA 1340 RBL 7.55 REPAIRED AFT PIT CARGO COMPARTMENT FLOOR STRINGER STA 1340 RBL 7.55 IAW B757 SRM 53-00-53-2RSDR FDEA202309031543Slat · delaminatedDISBOND INDICATION FOUND 5" OUTBOARD ON TOP SIDE OF SLAT #2 T/E WEDGE. REPAIRED #2 SLAT T/E WEDGE BY REMOVING DAMAGED AREA OS UPPER SKIN LOCATED 5.5" FROM I/B END AND 6.2" FROM TE AND BONDING REPAIR FILLER AND DOUBLER IAW B757 SRM 57- 43-02-2R AND 51-70-10-SDR FDEA202309031542Slat · delaminatedDISBOND INDICATION FOUND 93" OUTBOARD ON TOP SIDE OF SLAT #3 T/E WEDGE. REPAIRED #3 SALT T/E WEDGE UPPER SKIN DISBONDED AREA 93" FROM I/B END, 5375 FROM T/E IAW B757 SRM 57-43-02-2R FIG 201 REPAIR 1 AND 51-70-10-2R REPAIR 4SDR FDEA202309031541Slat · delaminatedDISBOND INDICATION FOUND 67" OUTBOARD ON TOP SIDE OF #3 TE WEDGE. REPAIRED #3 SLAT T/E UPPER SKIN DISBOND 67.5 FROM I/B END, 6.25" FROM T/E IAW B757 SRM 57- 43-02-2R FIG 201 REPAIR 1 AND 51-70-10-2R REPAIR 4.SDR FDEA202308291538Panel · crackedL.WING L/E PANEL 521AB HAS A CRACK AT THE EDGE OF THE PANEL EVALUATED, CLEANED, SANDED, REMOVED DAMAGE, ON L/E PANEL 521AB AND REPAIRED IAW B757 SRM 57-41-01-2R SRM 51-70-07, SRM 51-70-14SDR FDEA202303010354Guide Arm · failedENTRY DOOR WILL NOT CLOSE PROPERLY. APPEARS A HINGE IS NOT ALIGNED CORRECTLY. COMPLETED INSTALL OF L1 ENTRY DOOR GUIDE ARM. ALL ADJUSTMENTS AND OPS CHECKS GOOD. REF 757 AMM 52-11-04-2. RESDR FDEA202302220333None · nonePDIS 936 27-50 1303 22FEB23 MSP FACT U TE FLAP DISAGREE BETWEEN 5-15. RAN QRH AND LANDED MSP. ***EMERGENCY DECLARED*** FACT 22FEB23 13:11 MSP U FIM: 21-51-00-815-808 FIM: 21-51-00-815-815 UPON ENTERING FLIGHT DECK NOTED T/E AND L/E FLAPSDR FDEA202110252611Frame · unknownCOMPLY WITH EA FOR FRAME REPAIR STA. 1640 RH COMPLIED WITH EA #T F-5310-138502E P9 EA TITLE FUSELAGE-MAINFRAME-EXISTING FRAME REPAIR OF BS 1640, WL 208.10 RIGHT HAND-FRAME SECTION REPLACEMENT, CATEGORY "B" REPAIR, MAJOR REPAIR.SDR FDEA202110212587None · crackedCRACKED FLOOR BEAM @ STA. 580,LBL 45. REPAIRED FLOOR BEAM AT STA 580 LBL 45 PER E.A. # F-5310-T0364468 P1 AND SR DRAWING # 57-53-004 E.A. TITLE FUSELAGE-MAINFRAME-FLOOR BEAM AT STA. 580 AND LBL 45 CRACKED REPAIR PER DRAWING SR 57-53-004 WITH MINOR DEVIATIOSDR FDEA202110152541Seat Track · crackedSEAT TRACK AT STA 580, LBL 45, FLANGE HAS A CRACK. REPAIRED SEAT TRACK LBL45 AT STA 530 - 680 IAW EA# F-5321-T0364473, FUSELAGE - CARGO FLOOR - SECTION 43 - MCD SEAT TRACK FLANGE CRACK AT STA 580 LBL45. MAJOR REPAIRSDR FDEA202110082498None · damagedZONE 220 FLOOR BOARD 222MDF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MDF ON VT MAE TRAVELER T21/1575353 IAW DWG SRZ 25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082497None · damagedEDGE DAMAGE NOTED ON FLOOR PANEL 242MEF BOTTOM SIDE. FABRICATED FLOOR BOARD 242MEF ON VT MAE TRAVELER T21/1577548 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082496None · damagedZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T21/1575476 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082495None · damagedZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T21/1575357 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082494None · damagedZONE 220 FLOOR BOARD 222MEF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MEF ON VT MAE TRAVELER T21/1575352 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082493None · damagedZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T21/1575471 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082492None · damagedZONE 220 FLOOR BOARD 222BF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222BF ON VT MAE TRAVELER T21/1575359 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIRSDR FDEA202101090028Indicator · no indicationPRE-DEPARTURE UNABLE TO ARM L1 DOOR. NO SLIDE LIGHT. COMPLIED WITH INSPECTION & TEST OF GIRT BAR HANDING MECHANISM IAW MM 25-66-10-2. ALL CHECKED NORMAL . ARM LIGHT L1 DOOR TESTED NORMAL.. OK FOR SERVICE.SDR FDEA202011252964Transmission · trippedTRAILING EDGE FLAP DISAGREE BETWEEN 20&25 W/FLAP HANDLE IN 25 DETENT. COMPLIED W/QRH EMERGENCY DECLARED. ACCOMPLISHED FIM 27-51-00-815-808 FIG 105. FOUND RT INBOARD FLAP TRANS OVERLOAD INDICATION POPPED. RESET AND ACCOMPLISHED LUBE OF TRANS, PER AMM 12-21-SDR FDEA201910112605Cusp Web · corrodedMAIN CARGO AREA STA 1450 RH CUSP WEB CORRODED. REMOVED,FABRICATED AND INSTALLED NEW CUSP WEB IAW DWG 146N5590.SDR FDEA201910112604Skin · dentedEXTERIOR FUSELAGE SKIN DENTED AT STA 408 BETWEEN STRINGER 10L AND 11L REPAIRED PER EA# F-5310-T0349762-P1SDR FDEA201910112592Skin · dentedLOWER AFT CARGO FUSELAGE AT BS 1635 BETWEEN STR27R AND 28R HAS PITTING CORROSION ON INTERNAL SURFACE ACOMPLISHED WORK IAW EA F-5310-T0349844SDR FDEA2019101102590Slat Track · corrodedLEFT WING #3 SLAT INBD TRACK WORN AND PITTED. REMOVED AND REPLACED #3 SLAT IB MAINTRACK REF B757 AMM 27-81-12-4. ADJUSTMENT OF #3 TRACK IS ACCOMPLISHED ON NR N00107. OPS CHECK OF #3 SLAT MAIN TRACK IS ACCOMPLISHED ON NR N00107.SDR FDEA2019101102584Attach Angle · corrodedL/W L/E PNL ATTACH STRUCTURE AT STA 532 HAS INTERGRANULAR CORROSION REMOVED AND REPLACED ANGLE PER B757 SRM 51-40-02 AND DWG #114N2151SDR FDEA2019101102583Attach Angle · corrodedLEFT WING L/E PANEL ATTACH ANGLE AT WS 478 HAD INTERGRANULAR CORROSION. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02, AND DWG 114N2151.SDR FDEA201910092528Skin · corrodedLT WING NR 3 SLAT LEADING EDGE IS CORRODED APPROXIMATELY 32 IN OUTBOARD OF THE INBOARD EDGE IN THE UNPAINTED SURFACE. REPAIRED PER B757 SRM 57-43-01-2R.SDR FDEA2019101092528Skin · corrodedLEFT WING NR 3 SLAT L/E WAS CORRODED APPROX 32 INCHES OTBD OF THE INBD EDGE IN THE UNPAINTED SURFACE. REPAIRED THE SLAT IAW SRM 57-43-01-2R.SDR FDEA2019101092536Gear · corrodedLEFT WING NR 4 SLAT OTBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED NR 4 SLAT OTBD ROTARY ACTUATOR SPROCKET IAW AMM 27-81-18-4. OPS CHECKED GOOD IAW AMM 27-81-18-4.SDR FDEA201910092538Sprocket · corrodedLEFT WING NR 4 SLAT INBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED THE NR 4 SLAT INBD ROTARY ACTUATOR SPROCKET IAW AMM 57-81-18-4. OPS CHECKED GOOD IAW AMM 27-81-18-4.SDR FDEA2019101092537Sprocket · corrodedLEFT WING NR 3 SLAT INBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED NR 3 SLAT INBD ROTARY ACTUATOR SPROCKET IAW AMM 27-81-18-4. OPS CHECK GOOD IAW AMM 27-81-18-4.SDR FDEA2019101092533Slat Track · corrodedLEFT WING NR 3 SLAT OTBD TRACK WORN AND PITTED. REMOVED AND REPLACED THE NR 3 SLAT OTBD TRACK IAW AMM 27-81-12-4. OPS CHECKED GOOD IAW AMM 57-81, 81-18-4.SDR FDEA2019101092542Splice · corrodedLEFT WING T/E OTBD PANEL SPLICE STRIP, JUST AFT OF THE AILERON WAS CORRODED. REMOVED AND REPLACED THE SPLICE STRIP IAW SRM 51-40-02, AND DWG 113N1640, REV B.SDR FDEA2019101092539Striker · delaminatedLMLG DOOR AFT UPSTOP PAD IS WORN. REMOVED AND REPLACED STRIKER PLATE IAW SRM 51-10-02, DWG 149N6002, AND SRM 51-70-06-0G. REMOVED DAMAGED PLIES AND BONDED REPAIR IAW 5010, SRM 51-70-06-0G, AND SRM 52-80-02-2R. SEALED PLATE IAW SRM 51-20-05. RESTORED FINISH SDR FDEA2019101092535Striker · delaminatedRIGHT MLG DOOR LOWER UPSTOP PAD HAD COMPOSITE MATERIAL DELAMINATION. REMOVED DAMAGE AND STRIKER PLATE, BONDED NEW POTTING AND REPAIR PLIES AND STRIKER PLATE IAW DWG 149N6002, DWG 149N6003, REV C, SRM 51-70-06-0G, AND SRM 52-80-02-2R. SEALED PLATE IAW SRM 51-SDR FDEA2019101092532Slat Track · corrodedLEFT WING NR 4 SLAT INBD TRACK WORN AND PITTED. REMOVED AND REPLACED THE NR 4 SLAT INBOARD TRACK IAW AMM 27-81-12-4. ADJUSTMENT AND OPS CHECK ACCOMPLISHED ON SNRM N00108.SDR FDEA2019101092529Wedge · corrodedLEFT WING NR 5 SLAT LOWER T/E WEDGE WAS DELAMINATED AT THE INBD AFT CORNER. REPLACED THE SLAT.SDR FDEA2019101092527Attach Angle · corrodedRIGHT WING NR 9 SLAT LOWER T/E WEDGE ATTACH ANGLE IS CORRODED AND THE T/E WEDGE WAS BULGING WITH FASTENERS PULLING THROUGH AT THREE LOCATIONS. REPLACED THE SLAT.SDR FDEA2019101082502Skin · dentedAPU COMPARTMENT RT DOOR OUTER SURFACE IS CREASED. REPAIRED APU RT DOOR OUTER SKIN IAW EA F-5240-T0349703.SDR FDEA2019101082501Skin · dentedAPU COMPARTMENT LT DOOR OUTER SURFACE IS BULGED. REPAIRED APU DOOR OUTER SURFACE IAW EA F-5240-T0349685.SDR FDEA2019101082499Skin · dentedETERIOR FUSELAGE SKIN IS DENTED AT APPROX BS 1630 ON STR17R. REMOVED EFECTED FASTENERS PREFORMED HFEC TO OPEN HOLES AND EFECTED AREA FOUND NO CRACKS. OVERSIZED OPEN HOLES AND INSTALLED NEW FASTENERS IAW EA F-5330-T0349901.SDR FDEA201908091828Unknown · unknownMOD TYPE T MOD NO. F-5730-T0348437 REV NO. PS P2 WINGS - PLATES AND SKINS -
LH WING T.E. SKIN PANEL W BL 235 TO 300 - CRACKS AND
COMPLY WITH E..A. F-5730-T0348437 REV NO. POS.SDR FDEA201907081509Battery · dischargedDURING PRE-DEPARTURE CHECK, FOUND NUMEROUS EMERGENCY EXIT SIGNS AND R1 EXTERIOR LIGHT INOP. ATTEMPTED TO CHARGE EMERGENCY LIGHT BATTERIES USING SHIP'S POWER FOR 1 HOUR. NO HELP. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY ASSY IN REF TO AMM 33-51-07-2.
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