N357FE, cancelled Mar 2, 2024

Service difficulty reports · 195

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 = 'N357FE' AND deregistration_id = 'N357FE-2024-03-02'
  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.

SDR FDEA201909192282Slide · defectiveMDIS 357 25-60 5140 19SEP19 DFW OPEN U REF WRI 52-10/5139 L1 SLIDE INDICATOR ON ALL THE TIME. MEL 19SEP19 00:16 DFW U RELEASED FOR SERVICE PER MEL : 25-61-01 CATEGORY : C EXPIRATION : 29SEP19 "MEL 25-61-01: EVAC SLIDE REMOTE PRESS INDICATOR - INOPSep 19, 2019 · N357FE · Doug MD1010F · Emergency EquipmentSDR FDEA201901310235Switch · inoperativeON T/O AT ORD , NADPI T/O, ENGAGE PROF AT 500' AGL AT 1000' AGL NO PROF/GA THRUST AND SPEED SAW IT V2 PLUS 10 APPROX 165 KTS, PULLED LEVEL CHANGE. TRIED TO ENGAGE A/P BOUTIED 250 KTS AT 3000' A/C LEVELED AT 5000'. THEN STARTED DESCENT WHILE ACCELERATINJan 31, 2019 · N357FE · Doug MD1010F · Autopilot SystemSDR FDEA201807161725Control Panel · failedNR 2 ENGINE WOULD NOT RESTART AFTER BEING SHUTDOWN FOR A FUNCTIONAL TEST, INITIALLY ATTEMPTED AT FL 240 AND 250 KNOTS LATER AT 12000 AND 250 KNOTS, IN ALL CASES THE N1 WAS NORMAL, FUEL FLOW NORMAL, AND N2 WAS X OUT. FOUND OVERRIDE IGNTION SYSTEM INOP, REMOVEDJul 16, 2018 · N357FE · Doug MD1010F · Ignition SwitchingSDR FDEA201807161722Control Panel · failedNR 2 ENGINE WOULD NOT RESTART AFTER BEING SHUTDOWN FOR A FUNCTIONAL TEST. INITIALLY ATTEMPTED AT FL 240 AND 250 KNOTS LATER AT 12,000 AND 250 KNOTS. IN ALL CASES THE N, WAS NORMINAL, FUEL FLOW NORMAL AND N2 WAS "X" OUT. REMOVED AND REPLACED IGNITION CONTROL PAJul 16, 2018 · N357FE · Doug MD1010F · Engine CrankingSDR FDEA2018071641724Discharge Tube · dirtyDURING FUNCTIONAL CHECK OF NR 1 ENGINE. ENGINE WOULD NOT RESTART AFTER BEING INTENSIONALY SHUT DOWN. INITIALLY NOTED AT 250 KNOTS / 24,000. ATTEMPTED TO START SEVERAL MORE TIMES DOWN TO 12,000 NO HELP. N1 AND N2 NORMAL FUEL FLOW NORMAL, EGT NEVER SHOWED ANY RJul 14, 2018 · N357FE · Doug MD1010F · Engine Fuel and ControlSDR FDEA201807051635Skin · corrodedFABRICATE NEW DOUBLER AND ADD ADDITIONAL FASTENERS. REMOVED AND REPLACED DOUBLER PER EA 5330-T0340491 P1 AT STA 2020 RT SIDE BETWEEN L29 & L31. COMPLIED WITH WORK CARD EA T 8-5330-70340491 P1.Jul 5, 2018 · N357FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201807021621Angle · crackedNR 3 ACM COMPT CEILING AT STA 595 AND LONGERON 29 AIR LEAK FOUND DURING PRESSURIZATION. INSTALLED REPAIRED ANGLE IN REF TO SRM 53-40-00,VOL1 FIG 28 AT NR 3 ACM COMPT CEILING STA 595 AND LONGERON 29.Jul 2, 2018 · N357FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201806141489Hinge Fitting · worn3EA WEAR GOUGES ON INBOARD FLAP O/B HINGE WING ATTACHED HINGE. PERFORMED REPAIR FOR WEAR DAMAGE TO HINGE FITTING IAW SRM 57-20-00 FIG 17 V1.Jun 14, 2018 · N357FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201805301579Panel · corrodedMAIN DECK RT TOP AFT CENTER WING BOX PANEL HAS CORROSION AROUND FASTENER AT BS 1305, RBL 19, STRINGER 6 AT BUTT SPLICE. REPAIRED IN REF TO EA 8-5730-T0-340530, P1.May 30, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201805251589Panel · corrodedMAIN DECK, LT TOP OF AFT SLANT PANEL WAS SHOWING EXFOLIATION CORROSION AROUND FASTERNER HEADS AT BS 1346, LBL 106, STRINGER 2. REPAIRED IAW EA 8-5730-T0340530, P1, & SRM 57-20-00, FIG 8A, SHEETS 1 - 2, VOL 1.May 25, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA2018061251439Panel · corrodedMAIN DECK, LEFT TOP OF AFT SLANT PANEL WAS SHOWING EXFOLIATION CORROSION AROUND FASTERNER HEADS AT BS 1335, LBL 106, STRINGER 3. BLENDED AND REMOVED THE CORROSION. REPAIRED IAW EA 8-5730-T0340530, P1, & SRM 57-20-00, FIG 8A, SHEETS 1-2, VOL 1.May 25, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201805251581Panel · corrodedMAIN DECK, LT TOP OF AFT SLANT PANEL (CENTER WING BOX) IS SHOWING EXFOLIATION CORROSION AROUND FASTENER HEADS AT BS 1335, LBL 98, STRINGER 3. REF PREVIOUSLY GENERATED SNRM N00720. REPAIRED IN REFF TO EA 8-5730-T0340530, P1.May 25, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA2018053121337Seat Track · damagedMAIN CABIN SEAT TRACK AT BS 758 HAD BROKEN LOBES. REMOVED AND REPLACED THE SEAT TRACK SECTION IAW SRM 53-70-00, FIG 2, SHEETS 1-2, VOL 1.May 22, 2018 · N357FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805211477Spar Web · crackedNR 3 PYLON UPPER SPAR WEB HAS 21 EA HOLES WITH CRACK INDICATIONS. REMOVED AND REPLACED THE UPPER WEB TO AN UPGRADED WEB, IN REF TO EA 8-5450- T0340262, PART 1 ON THE NR 3 ENGINE, AFT OF THE TOMB STONE.May 21, 2018 · N357FE · Doug MD1010F · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201805171461Skin Splice · corrodedUPPER AUX TANK SKIN PANEL AT WS 1305, LONGERON 6, RBL 57, SKIN BUTT SPLICE IS HEAVILY CORRODED AROUND FASTENER HEAD. REPAIRED IAW EA 8-5730-T0340530, P1, & SRM 57-20-00, FIG 8A, VOL 1.May 17, 2018 · N357FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201805151310Floor Support · corrodedAFT LOWER CARGO BAY FLOOR SUPPORT HAD SURFACE CORROSION BS 1781 - 1860 ADJACENT AND ABOVE LATCH SPOOLS. REMOVED THE CORROSION IAW SRM 51-21-01.May 15, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201805151582Skin · corrodedMAIN DECK, STA 1315, RBL 98, TANK SURFACE, CORROSION, MARKED IN RED PENCIL. REPAIRED IN REF TO EA 8-5730-T0340530, P1.May 15, 2018 · N357FE · Doug MD1010F · Fuel StorageSDR FDEA201805151238Tee Fitting · crackedBS 595 BULKHEAD TEE VERTICAL LEG AT LONGERON 39R HAS A .300 INCH CRACK AT THE LOWER FASTENER. REPAIRED IAW DWG SR10530064-7013.May 15, 2018 · N357FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA2018052341308Bracket · crackedAFT CARGO DOOR SILL, FWD SPOOL SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-33-01 AND DWG AFA3150-501.May 14, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201805141549Fitting · crackedLT STA 1156 SUGAR SCOOP FITTING HAS A 2.0 IN CRACK BETWEEN LONG 38L-39L. REPAIRED SUGAR SCOOP FITTING CRACK REF SRM 53-40-00 FIG 8 VOL 1.May 14, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201805121490Attach Angle · crackedNR 3 PYLON INSIDE ACCESS PANEL488BL, LOOKING ACROSS AND AFT, ATTACH ANGLE TO TOMBSTONE FITTING TO PYLON SKIN IS CRACKED FIVE INCHES FROM TOP. WELDED DAMAGED AREA AS PER AMM 20-90-00-8 AND DPS 10.225 SECTIONS 4.8 TO 4.8.7 AND GENERAL WELD PROCEDURES 5.4 TO 5.5.May 12, 2018 · N357FE · Doug MD1010F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201805121441Web · crackedNR 1 PYLON INSIDE ACCESS PANEL 437CL, LT SIDE, STA YN210, PYLON WEB SKIN IS CRACKED APPROX TWO INCHES. REPAIR CRACKED PYLON WEB REF SRM 54-20-00 VOL 1 FIG 5A PAGE 20 AND SRM 51-33-01 VOL 2.May 12, 2018 · N357FE · Doug MD1010F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201805121316Web · crackedNOSE WHEEL WELL, BS 500, -Z=40. JUST FWD OF THE NR 3 PACK WW CUT OUT OPENING. THERE IS APPROXIMATELY A .250 INCH CRACK EMINATING FROM A RIVET HOLE. REPAIRED THE CRACKED AREA IAW SRM 53-30-00, FIG 6, PAGE 26, VOL.1.May 12, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201807031608Tee Fitting · crackedLT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONG 43L HAS A .300 INCH CRACK AT THE LOWER FASTENER. REPAIRED LT TEE-CAP REF EA 8-5310-T0340063 P1/P2.May 11, 2018 · N357FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201807031607Tee Fitting · crackedLT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONG 39L HAS A .800 INCH CRACK AT THE LOWER FASTENER. REPAIRED LT TEE-CAP REF EA 8-5310-T0340063 P1/P2.May 11, 2018 · N357FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201805111460Doubler · crackedRT WING INBOARD OF SLAT TRACK 9, PILLOW DOUBLER HAS CRACK. REPAIRED RT I/B SLAT TRACK 9 PILLOW DOUBLER CRACK PER SRM-57-10-00 FIG 71 VOL 1.May 11, 2018 · N357FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201805111459Doubler · crackedRT WING INBOARD OF SLAT TRACK 9, PILLOW DOUBLER HAS CRACK. REPAIRED RT I/B SLAT TRACK 9 PILLOW DOUBLER CRACK PER SRM-57-10-00 FIG 71 VOL 1.May 11, 2018 · N357FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201805101558Panel · delaminatedLT WING UPPER SURFACE INBD, TRAPEZOIDAL PANEL ARC0269. TOP SURFACE SHOWS SUSPECTED DELAMINATION AREA MARKED REPAIR PER SRM 57-71-00 VOL 2.May 10, 2018 · N357FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201805101443Skin · damagedFWD CARGO DOOR BOTTOM EDGE FWD OF AFT CORNER DAMAGE. REPAIR DAMAGED BOTTOM EDGE REF SRM 52-10-00 FIG 17 VOL 1.May 10, 2018 · N357FE · Doug MD1010F · Cargo/Baggage DoorsSDR FDEA201805101442Skin · damagedFWD CARGO DOOR AFT LOWER CORNER DAMAGE. REPAIR DAMAGED LOWER CORNER REF SRM 52-10-00 FIG 17 VOL 1.May 10, 2018 · N357FE · Doug MD1010F · Cargo/Baggage DoorsSDR FDEA2018053101363Skin · crackedRIGHT WING SKIN AT SLAT ANTI-ICE TELESCOPING DUCT CUTOUT, UPPER INBOARD CORNER HAD A .600 INCH CRACK AND UPPER OUTBOARD CORNER HAS A .300 IN. CRACK. REPAIRED IAW SRM 57-10-00, FIG 103, VOL 1.May 10, 2018 · N357FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201806051381Skin · crackedLEFT WING SKIN AT THE SLAT ANTI-ICE TELESCOPING DUCT CUTOUT, UPPER INBOARD CORNER HAS A .900 INCH CRACK AND UPPER OUTBOARD CORNER HAS A .500 INCH CRACK. REPAIRED THE LT WING SKIN AT SLAT ANTI-ICE TELESCOPING DUCT CUTOUT IAW SRM 57-10-00 FIG 103 SHEETS 1-6 VOLMay 10, 2018 · N357FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201805101258Seat Track · wornMAIN DECK COMPARTMENT - SEAT TRACK AT STA 889 RBL 110 IS WORN. REMOVED AND REPLACED SECTION OF SEAT TRACK (PLUG) IN REF TO SRM 53-70-00 FIG 2 SHEETS 1-2, VOL 1 AND SRM 51-30-01 VOL 2.May 10, 2018 · N357FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201804050856Valve · damagedDURING DESCENT FROM FL350 TO FL290, RECEIVED A TANK 3 TIP TRAPPED LEVEL 1 ALERT, WITH ASSOCIATED 5800 LBS UNUSABLE AND A TANK 3 PUMPS OFF ALERTS. PASSING 8000 FT, TRAPPED ALERT WENT AWAY, BUT THE NR 2 TANK KEPT FEEDING NR 3. INSPECTED TIP TANK TRANSFER SApr 5, 2018 · N357FE · Doug MD1010F · Fuel Quantity IndicatorSDR FDEA201802070313Float Valve · failed2.44 HRS INTO FLIGHT, RECEIVED A TANK 3 TIP TRAPPED LVL 1 ALERT. REMOVED & REPLACED INBD. TRANSFER FLOAT VALVE, NR 3 TANK IAW MM 28-21-10-2, & OPS. CHECKED NORMAL.Feb 7, 2018 · N357FE · Doug MD1010F · Fuel Indicating SystemSDR FDEA201611224184Power Supply · no testEMERGENCY BATTERY 1 LOW, ALERT DURING EMERGENCY LIGHTS TEST ON PREFLIGHT. TEST FAILED FOR POWER SUPPLY ASSY. REMOVED AND REPLACED THE POWER SUPPLY IAW MM 33-51-01-4 AND TESTED IAW MM 33-51-00-5. TEST PASSED. ACFT OK FOR SERVICE.Nov 22, 2016 · N357FE · Doug MD1010F · Emergency LightingSDR FDEA201607222599Landing Gear · malfunctionedLOWERED GEAR AT 220KTS TO AID IN DESCENT. WHEN GEAR WAS RAISED AT 220 KTS LEFT AND RIGHT MAIN GEAR INDICATED IN TRANSIT ON CONFIGURATION PAGE AND INDICATOR LIGHTS ABOVE GEAR HANDLE. RESEATED GEAR HANDLE WITH NO EFFECT. THERE WAS AIRFRAME VIBRATION AND Jul 22, 2016 · N357FE · Doug MD1010F · Landing Gear Retraction/Extension SystemSDR FDEA201606302206Light · inoperativeEMERGENCY LIGHTS ARE INOPERATIVE, TROUBLESHOT, 115VAC PRESENT AT PIN 6 & 5 OF P1-1756A, NO 28VDC AT PIN 8 OF P1-1756A, NO 28VDC AT TERMINAL D2 OF SWITCH S1-346. GOOD 28VDC COMING OFF C/B B1-907 EMERGENCY LIGHTS ARM UNABLE TO TROUBLESHOOT FURTHER TO FIND OPEN Jun 30, 2016 · N357FE · Doug DC1010F · Emergency LightingSDR FDEA201606292190Motor · failedL-1 DOOR WILL NOT FREE FALL WHEN ENGAGED. REPLACED L-1 DOOR ELECTRIC DRIVE MOTOR IAW AMM 52-11-01-2. OPS CHECK GOOD, PN 6322A0001-04, SN 1744.Jun 29, 2016 · N357FE · Doug MD1010F · Passenger/Crew DoorsSDR FDEA201605301761Wire · brokenR1 DOOR EMER DOOR SLIDE TEST SWITCH INOPERATIVE ON PRE-FLIGHT. RELEASED FOR SERVICE IAW MEL 25-61-01, CATEGORY C, EXPIRATION 03 JUN 16. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. FMay 30, 2016 · N357FE · Doug MD1010F · Equipment/Furnishings WiringSDR FDEA201605231718Panel · corrodedLEFT WING LOWER SURFACE FUEL VLV PANEL, LAND HAS EXFOLIATED CORROSION. CLEANED CORROSION & FABRICATED REPAIR DOUBLERS & FILLERS IAW 57-10-00.May 23, 2016 · N357FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201605221717Landing · crackedCRACK ON LT ACFT STRUCTURE PANEL 519AB LANDING FWD END, JUST INBD OF FUEL ACCESS PANEL. FABRICATED REPLACEMENT DOUBLER IAW DWG ARB 1180.May 22, 2016 · N357FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201605191673Stiffener · crackedCENTER WW FLOOR STIFFENER, CRACKED AT CTR LINE, APPROX STATION 1471. R & R IAW DWG AEA 0276-1 & SRM 51-31-01.May 19, 2016 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201605181653Skin · crackedLEFT WING FIXED LE ABOVE NR 1 PYLON, INBD OF SLAT NR 3 THERE IS A CRACK. INSTALLED FILLER & DOUBLER IAW SRM 57-00-01.May 18, 2016 · N357FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201605161587Door Frame · crackedR3 DOOR FWD JAMB, UPPER CORNER CRACKED. REMOVED DOUBLER, STOPPED DRILLED CRACK & INSTALLED NEW DOUBLER.May 16, 2016 · N357FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201605141583Skin · dentedLOWER FUSELAGE, SEVERAL DENTS IN OUTER SKIN LOCATED JUST FWD OF LOWER FWD CARGO DOOR, APPROX STATION 879, BETWEEN LONGERON 35 - 36. INSTALLED REPAIR IAW SRM 53-20-00 FIG 6.May 14, 2016 · N357FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201605051651Door Frame · crackedMAIN CABIN L3 DOOR, FWD DOOR JAMB, UPPER WEB CRACKED. REMOVED THE AEA 0530-19 DOUBLER & INSTALLED THE -7 REPAIR DOUBLER, STOP DRILLED CRACK IAW SRM 53-50-00 VOL I FIG 19 SHEET 1. FABRICATE NR 7 DOUBLER IAW SRM 53-50-00 FIG 19 7075-0 063 HEAT TREAT REQUIRED. May 5, 2016 · N357FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201605051533Seat Track · brokenMAIN CABIN SEAT TRACK HAS BROKEN LUG AT LOCK POSITION AT STATION 755, LBL 47 SPLICE IN NEW SECTION OF SEAT TRACK IAW SRM 53-70-00.May 5, 2016 · N357FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605041589Door Frame · crackedMAIN CABIN RT SIDE R3 DOOR AFT DOOR JAMB, UPPER CORNER CRACKED AT WEB. DRILL STOP CRACK, INSTALLED NEW 14 DOUBLER IAW SRM 53-50-00 VOL I FIG 19 SHEET 2 05 11 16. NDT TO VERIFY CRACK. COMPLIED WITH HFEC REF NDTSPM PART 06. VERIFIED & MARKED END OF CRACK. FMay 4, 2016 · N357FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201605031663Structure · crackedLEFT WING AT FIXED LE ABOVE NR 1 PYLON INBD OF SLAT, NR 3 THERE IS A CRACK. FABRICATED FILLER & DOUBLER IAW EA 8-5710-T0325356.May 3, 2016 · N357FE · Doug MD1010F · Wing Miscellaneous Structure
Back to N357FE, cancelled Mar 2, 2024