# Service difficulty reports: N357FE, cancelled Mar 2, 2024 A list on [N357FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N357FE-2024-03-02.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 4 · 195 reports - [SDR FDEA201909192282](https://openairdocs.org/sdr/FDEA201909192282.md): Slide · defective · Sep 19, 2019 · N357FE · Doug MD1010F · Emergency Equipment > MDIS 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 - INOP - [SDR FDEA201901310235](https://openairdocs.org/sdr/FDEA201901310235.md): Switch · inoperative · Jan 31, 2019 · N357FE · Doug MD1010F · Autopilot System > ON 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 ACCELERATIN - [SDR FDEA201807161725](https://openairdocs.org/sdr/FDEA201807161725.md): Control Panel · failed · Jul 16, 2018 · N357FE · Doug MD1010F · Ignition Switching > NR 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, REMOVED - [SDR FDEA201807161722](https://openairdocs.org/sdr/FDEA201807161722.md): Control Panel · failed · Jul 16, 2018 · N357FE · Doug MD1010F · Engine Cranking > NR 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 PA - [SDR FDEA2018071641724](https://openairdocs.org/sdr/FDEA2018071641724.md): Discharge Tube · dirty · Jul 14, 2018 · N357FE · Doug MD1010F · Engine Fuel and Control > DURING 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 R - [SDR FDEA201807051635](https://openairdocs.org/sdr/FDEA201807051635.md): Skin · corroded · Jul 5, 2018 · N357FE · Doug MD1010F · Fuselage Main, Plate/Skin > FABRICATE 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. - [SDR FDEA201807021621](https://openairdocs.org/sdr/FDEA201807021621.md): Angle · cracked · Jul 2, 2018 · N357FE · Doug MD1010F · Fuselage Main, Plate/Skin > NR 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. - [SDR FDEA201806141489](https://openairdocs.org/sdr/FDEA201806141489.md): Hinge Fitting · worn · Jun 14, 2018 · N357FE · Doug MD1010F · Trailing Edge Flaps > 3EA 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. - [SDR FDEA201805301579](https://openairdocs.org/sdr/FDEA201805301579.md): Panel · corroded · May 30, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous Structure > MAIN 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. - [SDR FDEA201805251589](https://openairdocs.org/sdr/FDEA201805251589.md): Panel · corroded · May 25, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous Structure > MAIN 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. - [SDR FDEA2018061251439](https://openairdocs.org/sdr/FDEA2018061251439.md): Panel · corroded · May 25, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous Structure > MAIN 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. - [SDR FDEA201805251581](https://openairdocs.org/sdr/FDEA201805251581.md): Panel · corroded · May 25, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous Structure > MAIN 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. - [SDR FDEA2018053121337](https://openairdocs.org/sdr/FDEA2018053121337.md): Seat Track · damaged · May 22, 2018 · N357FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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. - [SDR FDEA201805211477](https://openairdocs.org/sdr/FDEA201805211477.md): Spar Web · cracked · May 21, 2018 · N357FE · Doug MD1010F · Nacelle/Pylon, Frame/Spar/Rib > NR 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. - [SDR FDEA201805171461](https://openairdocs.org/sdr/FDEA201805171461.md): Skin Splice · corroded · May 17, 2018 · N357FE · Doug MD1010F · Wing, Plate/Skin > UPPER 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. - [SDR FDEA201805151310](https://openairdocs.org/sdr/FDEA201805151310.md): Floor Support · corroded · May 15, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous Structure > AFT LOWER CARGO BAY FLOOR SUPPORT HAD SURFACE CORROSION BS 1781 - 1860 ADJACENT AND ABOVE LATCH SPOOLS. REMOVED THE CORROSION IAW SRM 51-21-01. - [SDR FDEA201805151582](https://openairdocs.org/sdr/FDEA201805151582.md): Skin · corroded · May 15, 2018 · N357FE · Doug MD1010F · Fuel Storage > MAIN DECK, STA 1315, RBL 98, TANK SURFACE, CORROSION, MARKED IN RED PENCIL. REPAIRED IN REF TO EA 8-5730-T0340530, P1. - [SDR FDEA201805151238](https://openairdocs.org/sdr/FDEA201805151238.md): Tee Fitting · cracked · May 15, 2018 · N357FE · Doug MD1010F · Fuselage Main, Bulkhead > BS 595 BULKHEAD TEE VERTICAL LEG AT LONGERON 39R HAS A.300 INCH CRACK AT THE LOWER FASTENER. REPAIRED IAW DWG SR10530064-7013. - [SDR FDEA2018052341308](https://openairdocs.org/sdr/FDEA2018052341308.md): Bracket · cracked · May 14, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous Structure > AFT CARGO DOOR SILL, FWD SPOOL SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-33-01 AND DWG AFA3150-501. - [SDR FDEA201805141549](https://openairdocs.org/sdr/FDEA201805141549.md): Fitting · cracked · May 14, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous Structure > LT 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. - [SDR FDEA201805121490](https://openairdocs.org/sdr/FDEA201805121490.md): Attach Angle · cracked · May 12, 2018 · N357FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure > NR 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. - [SDR FDEA201805121441](https://openairdocs.org/sdr/FDEA201805121441.md): Web · cracked · May 12, 2018 · N357FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure > NR 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. - [SDR FDEA201805121316](https://openairdocs.org/sdr/FDEA201805121316.md): Web · cracked · May 12, 2018 · N357FE · Doug MD1010F · Fuselage Miscellaneous Structure > NOSE 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. - [SDR FDEA201807031608](https://openairdocs.org/sdr/FDEA201807031608.md): Tee Fitting · cracked · May 11, 2018 · N357FE · Doug MD1010F · Fuselage Main, Bulkhead > LT 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. - [SDR FDEA201807031607](https://openairdocs.org/sdr/FDEA201807031607.md): Tee Fitting · cracked · May 11, 2018 · N357FE · Doug MD1010F · Fuselage Main, Bulkhead > LT 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. - [SDR FDEA201805111460](https://openairdocs.org/sdr/FDEA201805111460.md): Doubler · cracked · May 11, 2018 · N357FE · Doug MD1010F · Leading Edge Devices > RT 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. - [SDR FDEA201805111459](https://openairdocs.org/sdr/FDEA201805111459.md): Doubler · cracked · May 11, 2018 · N357FE · Doug MD1010F · Leading Edge Devices > RT 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. - [SDR FDEA201805101558](https://openairdocs.org/sdr/FDEA201805101558.md): Panel · delaminated · May 10, 2018 · N357FE · Doug MD1010F · Wing, Plate/Skin > LT WING UPPER SURFACE INBD, TRAPEZOIDAL PANEL ARC0269. TOP SURFACE SHOWS SUSPECTED DELAMINATION AREA MARKED REPAIR PER SRM 57-71-00 VOL 2. - [SDR FDEA201805101443](https://openairdocs.org/sdr/FDEA201805101443.md): Skin · damaged · May 10, 2018 · N357FE · Doug MD1010F · Cargo/Baggage Doors > FWD CARGO DOOR BOTTOM EDGE FWD OF AFT CORNER DAMAGE. REPAIR DAMAGED BOTTOM EDGE REF SRM 52-10-00 FIG 17 VOL 1. - [SDR FDEA201805101442](https://openairdocs.org/sdr/FDEA201805101442.md): Skin · damaged · May 10, 2018 · N357FE · Doug MD1010F · Cargo/Baggage Doors > FWD CARGO DOOR AFT LOWER CORNER DAMAGE. REPAIR DAMAGED LOWER CORNER REF SRM 52-10-00 FIG 17 VOL 1. - [SDR FDEA2018053101363](https://openairdocs.org/sdr/FDEA2018053101363.md): Skin · cracked · May 10, 2018 · N357FE · Doug MD1010F · Wing, Plate/Skin > RIGHT 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. - [SDR FDEA201806051381](https://openairdocs.org/sdr/FDEA201806051381.md): Skin · cracked · May 10, 2018 · N357FE · Doug MD1010F · Wing, Plate/Skin > LEFT 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 VOL - [SDR FDEA201805101258](https://openairdocs.org/sdr/FDEA201805101258.md): Seat Track · worn · May 10, 2018 · N357FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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. - [SDR FDEA201804050856](https://openairdocs.org/sdr/FDEA201804050856.md): Valve · damaged · Apr 5, 2018 · N357FE · Doug MD1010F · Fuel Quantity Indicator > DURING 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 S - [SDR FDEA201802070313](https://openairdocs.org/sdr/FDEA201802070313.md): Float Valve · failed · Feb 7, 2018 · N357FE · Doug MD1010F · Fuel Indicating System > 2.44 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. - [SDR FDEA201611224184](https://openairdocs.org/sdr/FDEA201611224184.md): Power Supply · no test · Nov 22, 2016 · N357FE · Doug MD1010F · Emergency Lighting > EMERGENCY 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. - [SDR FDEA201607222599](https://openairdocs.org/sdr/FDEA201607222599.md): Landing Gear · malfunctioned · Jul 22, 2016 · N357FE · Doug MD1010F · Landing Gear Retraction/Extension System > LOWERED 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 - [SDR FDEA201606302206](https://openairdocs.org/sdr/FDEA201606302206.md): Light · inoperative · Jun 30, 2016 · N357FE · Doug DC1010F · Emergency Lighting > EMERGENCY 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 - [SDR FDEA201606292190](https://openairdocs.org/sdr/FDEA201606292190.md): Motor · failed · Jun 29, 2016 · N357FE · Doug MD1010F · Passenger/Crew Doors > L-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. - [SDR FDEA201605301761](https://openairdocs.org/sdr/FDEA201605301761.md): Wire · broken · May 30, 2016 · N357FE · Doug MD1010F · Equipment/Furnishings Wiring > R1 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. F - [SDR FDEA201605231718](https://openairdocs.org/sdr/FDEA201605231718.md): Panel · corroded · May 23, 2016 · N357FE · Doug MD1010F · Wing, Plate/Skin > LEFT WING LOWER SURFACE FUEL VLV PANEL, LAND HAS EXFOLIATED CORROSION. CLEANED CORROSION & FABRICATED REPAIR DOUBLERS & FILLERS IAW 57-10-00. - [SDR FDEA201605221717](https://openairdocs.org/sdr/FDEA201605221717.md): Landing · cracked · May 22, 2016 · N357FE · Doug MD1010F · Wing, Plate/Skin > CRACK ON LT ACFT STRUCTURE PANEL 519AB LANDING FWD END, JUST INBD OF FUEL ACCESS PANEL. FABRICATED REPLACEMENT DOUBLER IAW DWG ARB 1180. - [SDR FDEA201605191673](https://openairdocs.org/sdr/FDEA201605191673.md): Stiffener · cracked · May 19, 2016 · N357FE · Doug MD1010F · Fuselage Miscellaneous Structure > CENTER WW FLOOR STIFFENER, CRACKED AT CTR LINE, APPROX STATION 1471. R & R IAW DWG AEA 0276-1 & SRM 51-31-01. - [SDR FDEA201605181653](https://openairdocs.org/sdr/FDEA201605181653.md): Skin · cracked · May 18, 2016 · N357FE · Doug MD1010F · Wing, Plate/Skin > LEFT WING FIXED LE ABOVE NR 1 PYLON, INBD OF SLAT NR 3 THERE IS A CRACK. INSTALLED FILLER & DOUBLER IAW SRM 57-00-01. - [SDR FDEA201605161587](https://openairdocs.org/sdr/FDEA201605161587.md): Door Frame · cracked · May 16, 2016 · N357FE · Doug MD1010F · Fuselage Main, Structure > R3 DOOR FWD JAMB, UPPER CORNER CRACKED. REMOVED DOUBLER, STOPPED DRILLED CRACK & INSTALLED NEW DOUBLER. - [SDR FDEA201605141583](https://openairdocs.org/sdr/FDEA201605141583.md): Skin · dented · May 14, 2016 · N357FE · Doug MD1010F · Fuselage Main, Plate/Skin > LOWER 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. - [SDR FDEA201605051651](https://openairdocs.org/sdr/FDEA201605051651.md): Door Frame · cracked · May 5, 2016 · N357FE · Doug MD1010F · Fuselage Main, Structure > MAIN 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. - [SDR FDEA201605051533](https://openairdocs.org/sdr/FDEA201605051533.md): Seat Track · broken · May 5, 2016 · N357FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings > MAIN 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. - [SDR FDEA201605041589](https://openairdocs.org/sdr/FDEA201605041589.md): Door Frame · cracked · May 4, 2016 · N357FE · Doug MD1010F · Fuselage Main, Structure > MAIN 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. F - [SDR FDEA201605031663](https://openairdocs.org/sdr/FDEA201605031663.md): Structure · cracked · May 3, 2016 · N357FE · Doug MD1010F · Wing Miscellaneous Structure > LEFT 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. Next page: https://openairdocs.org/deregistered/N357FE-2024-03-02/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N357FE-2024-03-02/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.