N10060, cancelled Mar 2, 2024

Service difficulty reports · 235

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 = 'N10060' AND deregistration_id = 'N10060-2024-03-02'
  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 FDEA202004130737Static Wick · out of tolerancePDIS 060 23-10 4976 13APR20 FLL FACT U LOGPAGES:3208974 LOST ALL THREE COM'S PASSING THRU FL310. AFTER PASSING FL350 #1 STARTED TO WORK, ONE BY ONE THEN ON OTHER SIDE OF STORM ALL THREE STARTED TO WORK NORMAL.HEADSET ON CAPT'S SIDE CAN'T TRANApr 13, 2020 · N10060 · Doug MD1010F · Static Discharge SystemSDR FDEA201909072149Via · malfunctionedDURING TAKEOFF ROLL SEVERAL OF THE DU'S STARTED TO FLASH ON AND OFF. ALSO RECEIVED A CONFIGURATION WARNING. ABORTED TAKEOFF AT APPOX 90 KTS. R&R #3 VIA PRECAUTIONARILY - OPS CHK GOOD. REF 31-43-01-4.Sep 7, 2019 · N10060 · Doug MD1010F · Central ComputersSDR FDEA201905020983Warning System · false activationRECEIVED LEVEL 1 ALERT "AIR SYS 2 OFF". 2 MINUTES LATER RECEIVED LEVEL 3 ALERT "AIR MANF 2 FAIL". RAN QRH. LEVEL 3 ALERT EXTINGUISHED WHEN NR 2 THROTTLE PULLED TO IDLE VIA QRH DIRECTION. RESTORED MEL DEACTIVATIONS TO NORMAL CONFIG PERFORMED AIR SYSTEM TEST WIMay 2, 2019 · N10060 · Doug MD1010F · Pneumatic Indicating SystemSDR FDEA201812270126Stringer · damagedLT STA.1156 HAS AN OVERSIZE HOLE REF PART # ARB0323-1 REPAIR WILL BE REPAIRED ON E.A. 8-5310-T0344334 REPAIRED PER EA#8-5310-T0344334 FUSELAGE-MAINFRAME-STA.1156 BLKHD TEE CAP- OVERSIZED HOLES REPAIR.Dec 27, 2018 · N10060 · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201812263609Support · corrodedVERTICAL STAB, BOTTOM SUPPORT BRACE FOR PANEL 374FR IS CORRODED. REPLACED BOTTOM SUPPORT WITH NEW SERVICEABLE SUPPORT ANGLE PER MD-10 SRM 51- 31-01 VOL. 2. AND DOUGLAS DRAWING AMC7202.Dec 26, 2018 · N10060 · Doug MD1010F · Vertical StabilizerSDR FDEA2018121083483Skin · damagedL/H WING, #3 SPOILER, UPPER SURFACE AT STA. XOSP3 609, HAS AN EXISTING SKIN DOUBLER, APPROX. 4' DIA. REPAIRE PER SRM 57-00-01 FIG.4 SHT.1Dec 8, 2018 · N10060 · Doug MD1010F · SpoilersSDR FDEA201811303403Skin · damaged[R/H WING, I/B FLAP HAS DAMAGE ON TOP OF SKIN BY STA. XIFH 155., 2018-11-30] REPAIRED THE R/H WING, I/B FLAP UPPER SURFACE PER SRM 57-10-00 FIG 85 SHEET 4 VOL 1 & TRACKING EA # 8-5710-T0343639, PART 3Nov 30, 2018 · N10060 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201811303399Skin · damaged[RH INBD FLAP DAMAGED ON TOP SIDE OF FLAP., 2018-11-30] REPAIRED DAMAGE ON THE R/H FLAP, UPPER SURFACE PER SRM 57-10-00 FIG 85 SHEET 4 VOL1 & TRACKING EA # 8-5710-T0343639, PART 2Nov 30, 2018 · N10060 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201811303397Skin · gouged[R/H WING I/B FLAP...TOP FWD SURFACE..APPROX C/L....WEAR MARK/GOUGE ON FLAP SKIN... REFERENCE...SNRM #203, 2018-11-30] REPAIRED THE DAMAGE PER SRM 57-10-00 FIG 85 SHEET 4 VOL 1 & R.S.C. TRACKING EA # 8-5710-T0343639, PART 1Nov 30, 2018 · N10060 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201811280209Spar · out of alignmentRT HORIZ SPAR CAP BARREL NUT BOLT HOLE IS MISALIGNED. REPAIRED PER EA 8-5510-T0343409 "HORIZONTAL STABILIZER- RT UPPER REAR SPAR REPAIR"Nov 28, 2018 · N10060 · Doug MD1010F · Horizontal Stabilizer, Spar/RibSDR FDEA201811270125Fitting · crackedLT STA. 1156 FWD HOZ LEG HAS 4 EA. OPEN HOLES BETWEEN LONGERON 38L-39L IN SKIN AND AYB7000-1 FITTING AND 1 EA. OPEN HOLE ON AFT HORZ LEG IN SKIN HAVE CRACK INDICATIONS. REPAIRED PER EA # 8-5310-T0344334 FUSELAGE- MAINFRAME-STA.1156 BLKHD TEE CAP- OVERSIZED HONov 27, 2018 · N10060 · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201811273417Floor Support · corrodedMAIN DECK FLOOR SUPPORT ATTACHED ANGLE CLIP IS SHOW SIGN OF CORROSION AT STATION 1972 RBL40. INSTALLED NEW FLOOR SUPPORT AGA7091-50 PER DWG AGA7091 REF SRM 51-35-01 VOL 2.Nov 27, 2018 · N10060 · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201811273416Floor Support · corrodedMAIN DECK FLOOR SUPPORT ATTACHED ANGLE CLIP IS SHOW SIGN OF CORROSION AT STATION 1972 LBL40. INSTALLED NEW FLOOR SUPPORT AGA7091-49 PER DWG AGA7091 REF SRM 51-35-01 VOL 2.Nov 27, 2018 · N10060 · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201811153476Skin · crackedRT WING LE INTERNAL STRUCTURE BEADED DOUBLER CRACKED, THREE (3) PLACES, LOCATION APPROX XORS 817, OUTBD OF NR 14 SLAT TRACK, ACCESS THROUGH FUEL VALVE PANEL 626FB. CRACK LENGTHS APPROX 1.00", .500" AND .250". CRACKS CONFIRMED AND ENDS MARKED USING NDT HFEC. RENov 15, 2018 · N10060 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201811143429Floor Panel · delaminatedMAIN CABIN, STA 435 - 475 FLOOR IS SPONGY AND DELAMINATED. FABRICATED NEW FLOOR PANEL 225BF, STA 435 TO STA 475 REF DWG SRZ-25-005.Nov 14, 2018 · N10060 · Doug MD1010F · Fuselage Floor PanelSDR FDEA201811133430Floor Support · crackedMAIN DECK FLOOR SUPPORT ATTACHED ANGLE CLIP IS SHOW SIGN OF CRACKED AT STA 455 RBL 10. REPLACED FLOOR SUPPORT ABA7423-1 PER SRM 51-31-01 VOL 2, AND DWG ABA7423.Nov 13, 2018 · N10060 · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201811113437Fitting · crackedRIGHT WING LEADING EDGE STA 1159 AT APPROX LONG 30 T-CAP ANGLE FITTING IS CRACKED MARKED 23 STATION 1159 RBL. LONG 30 AT LEADING EDGE REMOVED AND REPLACED T-CAP ANGLE FITTING PER SRM 57-20-00 FIG. 6 SHEET 3-503 FRONT SPA TO FRAME REPAIR. ALSO IN CONJUNCTION WNov 11, 2018 · N10060 · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201811113415Seat Track · corrodedMAIN CARGO COMPT CENTER FLOOR SUPPORT APPROX STA 392 TO 435, X=0. FLOOR SUPPORT SHOWS CORROSION. INSTALLED NEW SEAT TRACK PER SRM 51-31-01 VOL 2 AND DAC DWG NBA6018.Nov 11, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201811113412Seat Track · corrodedMAIN CARGO COMPT APPROX STA 455 TO 475, X=-47.50 SEAT TRACK CHANNEL CORRODED. INSTALLED SEAT TRACK PER SRM 51-31-01 VOL 2 AND DRAWING NBA6018.Nov 11, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201811113391Seat Track · corrodedMAIN CARGO COMPT: APPROX STA 435 TO 455, X=-8.50 SEAT TRACK SHOWS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT SEAT TRACK IN MAIN CARGO COMPT APPROX STATION 435-485, RBL 8.5 REF SRM 53-70-00 FIG 1 VOL 1 AND SRM 51-31-01 VOL 2 AND DWG SR10-53-002 AND DAC DWG NNov 11, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201811113387Seat Track · corrodedMAIN CARGO COMPT: APPROX STA 435 TO 455, X=8.50 FLOOR SUPPORT SEAT TRACK SHOWS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT SEAT TRACK IN MAIN CARGO COMPT APPROX STATION 435-485, LBL 8.5 REF SRM 53-70-00 FIG 1 VOL 1 AND SRM 51-31-01 VOL 2 AND DWG SR10-53-002 Nov 11, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201811093386Floor Panel · damagedMAIN DECK- FOUND EXISTENT FLOOR PANEL REPAIR IS COMING OFF AT STA 775 LBL 100. FABRICATED NEW FLOOR PNL AT STA 775 LBL 100 REF DWG SRZ-25-005.Nov 9, 2018 · N10060 · Doug MD1010F · Fuselage Floor PanelSDR FDEA201811093271Skin · none#3 AIR COND. COMPT. DOOR, STA. 496-525, HAS AN EXISTING DOUBLER ON TOP EDGE. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 52-10-00 FIG. 2, SHT. 2, VOL. 1.Nov 9, 2018 · N10060 · Doug MD1010F · Air Conditioning DoorsSDR FDEA201811093171Floorboard · corrodedMAIN CABIN FLOORBOARD SHOWS EVIDENCE OF CORROSION, STA 435 TO STA 475 AT RBL 17 AND NEEDS TO BE REPLACED. REMOVED AND REPLACED FLOORBOARD IN REF TO DWG SRZ-25-005.Nov 9, 2018 · N10060 · Doug MD1010F · Fuselage Floor PanelSDR FDEA201811093169Floorboard · corrodedMAIN CABIN FLOORBOARD DELAMINATED, STA 475 TO STA 495 AT RBL 17 AND NEEDS TO BE REPLACED. REMOVED AND REPLACED FLOORBOARD IN REF TO DWG SRZ-25-005.Nov 9, 2018 · N10060 · Doug MD1010F · Fuselage Floor PanelSDR FDEA2018110983129Skin · crackedR/H FUSELAGE SKIN AT STA. 1156 HAS A .400 IN. CRACK AT THE AFT FASTENER HOLE COMMON TO THE TEE CAP (2 FASTENERS ABOVE LONGERON 39R) PROPAGATING AFT TO THE EDGE OF SKIN PANEL. (MARKED) WORKED I.A.W E.A # 8-5310-T0343606 (FUSELAGE-MAINFRAME-FUSELAGE SKIN ANDNov 8, 2018 · N10060 · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201811073377Seat Track · wornMAIN DECK COMPT STA1260 48RBL SEAT TRACK LOBE WORN. REMOVED AND REPLACED SEAT TRACK ON MAIN DECK COMPT AT EXISTING SPLICE FROM APPROX STATION 1246 TO STATION 1330, 48 RBL REF SRM 53-70-00 FIG 1 VOL 1, SRM 51-31-01 VOL 2 AND DWG SR10-53-002.Nov 7, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201811073317Seat Track · wornMAIN DECK COMPT STA1260 48LBL SEAT TRACK LOBE WORN (MARKED) INSTALLED AND SEAL NEW SEAT TRACK REF. SRM 53-70-00 FIG. 1 VOL. 1 AND SRM 51-31-01 VOL. 2.Nov 7, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018111973303Seat Track · wornMAIN DECK COMPT STA1541 22RBL SEAT TRACK LOBE WORN (MARKED) REPLACED DAMAGED SECTION OF SEAT TRACK FROM STATION 1541 TO STATION 1581. REFERENCE SRM 53-70-00 FIGURE 1 VOL 1 .Nov 7, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201811073186Floor Support · corrodedMAIN DECK STA 735 LBL 28-48 FLOOR BOARD SUPPORT HAS CORROSION DAMAGE. REMOVE AN REPLACED NEWLY FABRICATED FLOOR BOARD SUPPORT ACA7417-17 STA 735 LBL 28-48. REF DRAWING ACA7417.Nov 7, 2018 · N10060 · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201811073118Spar Cap · crackedRT HORIZONTAL STAB, OUTER SECTION UPPER AFT SPAR CAP HAS A CRACK APPROX .400" LONG ORIGINATING AFT OF AFT BARREL NUT HOLE CONTINUING TO AFT EDGE OF SPAR CAP. REPAIRED RT HORIZ STAB SPAR ER EA 8-5510-T0343409 REF SEQ 827 W/O 72895 MAJOR REPAIR.Nov 7, 2018 · N10060 · Doug MD1010F · Horizontal Stabilizer, Spar/RibSDR FDEA2018111963306Skin · corrodedRH WING UPPER SURFACE APPROX XORS 264 STRINGER 12 - CORROSION AROUND FASTENER. REMOVED CORROSION AT APPROX XORS264 STRINGER 12 RH WING UPPER SURFACE AROUND FASTENER REF MD10 SRM 57-10-00 VOL1 FIG 60 SHT 1 MATERIAL REMOVED WAS APPROX .028 MAX ALLOWED IS .Nov 6, 2018 · N10060 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201711183272Apu · smokeAPU SMOKE. APU SHUTDOWN (AUTO). OBSERVED SMOKE FROM APU. DEPLOYED FIRE AGENT TO APU.Nov 18, 2017 · N10060 · Doug MD1010F · Airborne Auxiliary Power Unit (APU) SystemSDR FDEA201611013784Tee Fitting · crackedBS 1156 BULKHEAD TEE FITTING VERTICAL LEG CRACKED ABOVE LONGERON 39L. REPAIRED IAW EA 8-5310-T0328855Nov 1, 2016 · N10060 · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201610193663Web · crackedNR 3 PYLON UPPER WEB OTBD SIDE HAS A CRACK INDICATION. REPAIRED IAW EA 8-5400-T0329061.Oct 19, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201610193662Fitting · crackedNR 3 PYLON AFT BULKHEAD FITTING HAS A CRACK INDICATION AT THE FOURTH HOLE FROM OTBD SIDE. REPAIRED IAW EA 8-5400-T0329061.Oct 19, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon, Main FrameSDR FDEA201610193661Bolt · looseNR 3 PYLON, UPPER AFT SECTION OF SPAR WEB, HAS 15 LOOSE BOLTS. REAMED HOLES TO FIRST OVERSIZE AND INSTALLED B/P BOLTS IAW SRM 54-20-00 F. 27, VOL IOct 19, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon, Main FrameSDR FDEA201610183652Web · crackedNR 3 PYLON, UPPERWEB , FOUND CRACK APPROX 1.75 INCH FROM EDGE OF UPPER SPAR WEB THRU 1 FASTENER HOLE TERMINATING AT I/B FASTENER HOLE OF AUB7031-11 DOUBLER. R&R WEB PER EA 8-5400--T0329061 AND SB 54-90.Oct 18, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201610173646Skin · crackedRT WING STAT TRACK NR 14 CUT OUT AFT O/B CORNER HAS A .300 IN CRACK. INSTALLED A DOUBLER PER SRM 57-10-00 FIG 68 VOL 1.Oct 17, 2016 · N10060 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201610173645Skin · crackedRT WING STAT TRACK NR 14 CUT OUT AFT O/B CORNER HAS A .300 IN CRACK. INSTALLED A DOUBLER PER SRM 57-10-00 FIG 68 VOL 1.Oct 17, 2016 · N10060 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201610133609Skin · wornRT WING LOWER LEADING EDGE, AREAS COMMON TO PYLON, SKIN IS WORN. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 87.Oct 13, 2016 · N10060 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201610123548Skin · delaminatedRIGHT WING INBD FLAP O/B HINGE PANEL 641CR DELAMINATED. REPAIRED THE DAMAGE IAW SRM 51-71-00 VOL IIOct 12, 2016 · N10060 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201610113544Skin · dentedRIGHT ELEVATOR LOWER SURFACE CREASED. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 55-10-00 FIG. 8 VOL. IOct 11, 2016 · N10060 · Doug MD1010F · Elevator, Plate/SkinSDR FDEA201610043455Floorbeam · corrodedAFT CARGO BAY BS 1841 FLOORBEAM HAS SEVERAL AREAS WITH CORROSION. LBL TO RBL 18. REPAIRED IAW DWG AGA3874Oct 4, 2016 · N10060 · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201610033647Acoustic Panel · crackedNR 1 ENGINE NOSE COWL AT 12 O'CLOCK POSITION BETWEEN NOSE COWL LEADING EDGE AND ACOUSTIC PANEL HAS A CRACK. INSTALLED REPAIR DOUBLER PER SRM 54-11-00 FIG 1A.Oct 3, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201610033528Roller Tray · crackedFWD CARGO ROLLER TRAY AT BS 920 DOOR ENTRY AREA CRACKED. REPLACED THE ROLLER TRAY IAW NDJ6030.Oct 3, 2016 · N10060 · Doug MD1010F · Cargo CompartmentsSDR FDEA201610023428Tee Fitting · crackedRT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R HAS A .5 IN CRACK AT THE LOWER FASTENER. REPAIRED IAW EA 8-5310-T0328704.Oct 2, 2016 · N10060 · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201610023427Tee Fitting · crackedRT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39R HAS A .5 IN CRACK AT THE UPPER AND LWR FASTENER. REPAIRED IAW EA 8-5310-T0328704.Oct 2, 2016 · N10060 · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201610023426Tee Fitting · crackedLEFT BS 595 BULKHEAD TEE CAP AT LONGERON 39L HAS A .5 IN CRACK AT THE LWR FASTENER. REPAIRED IAW EA 8-5310-T0328709.Oct 2, 2016 · N10060 · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201610013904Bolt · shearedNR 3 PYLON UPPER WEB SURFACE OTBD SIDE, ALONG THE EDGE HAS A SHEARED BOLT. REPAIRED IAW EA 8-5400-T0329061 AND SRM 54-20-00 FIG. 27, VOL. I.Oct 1, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon, Main Frame
Back to N10060, cancelled Mar 2, 2024