# Service difficulty reports: N10060, cancelled Mar 2, 2024

A list on [N10060, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N10060-2024-03-02.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 5 · 235 reports

- [SDR FDEA202004130737](https://openairdocs.org/sdr/FDEA202004130737.md): Static Wick · out of tolerance · Apr 13, 2020 · N10060 · Doug MD1010F · Static Discharge System
  > PDIS 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 TRAN
- [SDR FDEA201909072149](https://openairdocs.org/sdr/FDEA201909072149.md): Via · malfunctioned · Sep 7, 2019 · N10060 · Doug MD1010F · Central Computers
  > DURING 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.
- [SDR FDEA201905020983](https://openairdocs.org/sdr/FDEA201905020983.md): Warning System · false activation · May 2, 2019 · N10060 · Doug MD1010F · Pneumatic Indicating System
  > RECEIVED 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 WI
- [SDR FDEA201812270126](https://openairdocs.org/sdr/FDEA201812270126.md): Stringer · damaged · Dec 27, 2018 · N10060 · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > LT 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.
- [SDR FDEA201812263609](https://openairdocs.org/sdr/FDEA201812263609.md): Support · corroded · Dec 26, 2018 · N10060 · Doug MD1010F · Vertical Stabilizer
  > VERTICAL 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.
- [SDR FDEA2018121083483](https://openairdocs.org/sdr/FDEA2018121083483.md): Skin · damaged · Dec 8, 2018 · N10060 · Doug MD1010F · Spoilers
  > L/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.1
- [SDR FDEA201811303403](https://openairdocs.org/sdr/FDEA201811303403.md): Skin · damaged · Nov 30, 2018 · N10060 · Doug MD1010F · Trailing Edge Flaps
  > [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 3
- [SDR FDEA201811303399](https://openairdocs.org/sdr/FDEA201811303399.md): Skin · damaged · Nov 30, 2018 · N10060 · Doug MD1010F · Trailing Edge Flaps
  > [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 2
- [SDR FDEA201811303397](https://openairdocs.org/sdr/FDEA201811303397.md): Skin · gouged · Nov 30, 2018 · N10060 · Doug MD1010F · Trailing Edge Flaps
  > [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 1
- [SDR FDEA201811280209](https://openairdocs.org/sdr/FDEA201811280209.md): Spar · out of alignment · Nov 28, 2018 · N10060 · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > RT HORIZ SPAR CAP BARREL NUT BOLT HOLE IS MISALIGNED. REPAIRED PER EA 8-5510-T0343409 "HORIZONTAL STABILIZER- RT UPPER REAR SPAR REPAIR"
- [SDR FDEA201811270125](https://openairdocs.org/sdr/FDEA201811270125.md): Fitting · cracked · Nov 27, 2018 · N10060 · Doug MD1010F · Fuselage Miscellaneous Structure
  > LT 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 HO
- [SDR FDEA201811273417](https://openairdocs.org/sdr/FDEA201811273417.md): Floor Support · corroded · Nov 27, 2018 · N10060 · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR FDEA201811273416](https://openairdocs.org/sdr/FDEA201811273416.md): Floor Support · corroded · Nov 27, 2018 · N10060 · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR FDEA201811153476](https://openairdocs.org/sdr/FDEA201811153476.md): Skin · cracked · Nov 15, 2018 · N10060 · Doug MD1010F · Wing, Plate/Skin
  > RT 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. RE
- [SDR FDEA201811143429](https://openairdocs.org/sdr/FDEA201811143429.md): Floor Panel · delaminated · Nov 14, 2018 · N10060 · Doug MD1010F · Fuselage Floor Panel
  > MAIN CABIN, STA 435 - 475 FLOOR IS SPONGY AND DELAMINATED. FABRICATED NEW FLOOR PANEL 225BF, STA 435 TO STA 475 REF DWG SRZ-25-005.
- [SDR FDEA201811133430](https://openairdocs.org/sdr/FDEA201811133430.md): Floor Support · cracked · Nov 13, 2018 · N10060 · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR FDEA201811113437](https://openairdocs.org/sdr/FDEA201811113437.md): Fitting · cracked · Nov 11, 2018 · N10060 · Doug MD1010F · Wing Miscellaneous Structure
  > RIGHT 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 W
- [SDR FDEA201811113415](https://openairdocs.org/sdr/FDEA201811113415.md): Seat Track · corroded · Nov 11, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR FDEA201811113412](https://openairdocs.org/sdr/FDEA201811113412.md): Seat Track · corroded · Nov 11, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR FDEA201811113391](https://openairdocs.org/sdr/FDEA201811113391.md): Seat Track · corroded · Nov 11, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 N
- [SDR FDEA201811113387](https://openairdocs.org/sdr/FDEA201811113387.md): Seat Track · corroded · Nov 11, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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
- [SDR FDEA201811093386](https://openairdocs.org/sdr/FDEA201811093386.md): Floor Panel · damaged · Nov 9, 2018 · N10060 · Doug MD1010F · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA201811093271](https://openairdocs.org/sdr/FDEA201811093271.md): Skin · none · Nov 9, 2018 · N10060 · Doug MD1010F · Air Conditioning Doors
  > #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.
- [SDR FDEA201811093171](https://openairdocs.org/sdr/FDEA201811093171.md): Floorboard · corroded · Nov 9, 2018 · N10060 · Doug MD1010F · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA201811093169](https://openairdocs.org/sdr/FDEA201811093169.md): Floorboard · corroded · Nov 9, 2018 · N10060 · Doug MD1010F · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA2018110983129](https://openairdocs.org/sdr/FDEA2018110983129.md): Skin · cracked · Nov 8, 2018 · N10060 · Doug MD1010F · Fuselage Main, Plate/Skin
  > R/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 AND
- [SDR FDEA201811073377](https://openairdocs.org/sdr/FDEA201811073377.md): Seat Track · worn · Nov 7, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR FDEA201811073317](https://openairdocs.org/sdr/FDEA201811073317.md): Seat Track · worn · Nov 7, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR FDEA2018111973303](https://openairdocs.org/sdr/FDEA2018111973303.md): Seat Track · worn · Nov 7, 2018 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR FDEA201811073186](https://openairdocs.org/sdr/FDEA201811073186.md): Floor Support · corroded · Nov 7, 2018 · N10060 · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR FDEA201811073118](https://openairdocs.org/sdr/FDEA201811073118.md): Spar Cap · cracked · Nov 7, 2018 · N10060 · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > RT 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.
- [SDR FDEA2018111963306](https://openairdocs.org/sdr/FDEA2018111963306.md): Skin · corroded · Nov 6, 2018 · N10060 · Doug MD1010F · Wing, Plate/Skin
  > RH 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.
- [SDR FDEA201711183272](https://openairdocs.org/sdr/FDEA201711183272.md): Apu · smoke · Nov 18, 2017 · N10060 · Doug MD1010F · Airborne Auxiliary Power Unit (APU) System
  > APU SMOKE. APU SHUTDOWN (AUTO). OBSERVED SMOKE FROM APU. DEPLOYED FIRE AGENT TO APU.
- [SDR FDEA201611013784](https://openairdocs.org/sdr/FDEA201611013784.md): Tee Fitting · cracked · Nov 1, 2016 · N10060 · Doug MD1010F · Fuselage Main, Bulkhead
  > BS 1156 BULKHEAD TEE FITTING VERTICAL LEG CRACKED ABOVE LONGERON 39L. REPAIRED IAW EA 8-5310-T0328855
- [SDR FDEA201610193663](https://openairdocs.org/sdr/FDEA201610193663.md): Web · cracked · Oct 19, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon, Bulkhead/Firewall
  > NR 3 PYLON UPPER WEB OTBD SIDE HAS A CRACK INDICATION. REPAIRED IAW EA 8-5400-T0329061.
- [SDR FDEA201610193662](https://openairdocs.org/sdr/FDEA201610193662.md): Fitting · cracked · Oct 19, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon, Main Frame
  > NR 3 PYLON AFT BULKHEAD FITTING HAS A CRACK INDICATION AT THE FOURTH HOLE FROM OTBD SIDE. REPAIRED IAW EA 8-5400-T0329061.
- [SDR FDEA201610193661](https://openairdocs.org/sdr/FDEA201610193661.md): Bolt · loose · Oct 19, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon, Main Frame
  > NR 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 I
- [SDR FDEA201610183652](https://openairdocs.org/sdr/FDEA201610183652.md): Web · cracked · Oct 18, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NR 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.
- [SDR FDEA201610173646](https://openairdocs.org/sdr/FDEA201610173646.md): Skin · cracked · Oct 17, 2016 · N10060 · Doug MD1010F · Wing, Plate/Skin
  > RT 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.
- [SDR FDEA201610173645](https://openairdocs.org/sdr/FDEA201610173645.md): Skin · cracked · Oct 17, 2016 · N10060 · Doug MD1010F · Wing, Plate/Skin
  > RT 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.
- [SDR FDEA201610133609](https://openairdocs.org/sdr/FDEA201610133609.md): Skin · worn · Oct 13, 2016 · N10060 · Doug MD1010F · Wing, Plate/Skin
  > RT WING LOWER LEADING EDGE, AREAS COMMON TO PYLON, SKIN IS WORN. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 87.
- [SDR FDEA201610123548](https://openairdocs.org/sdr/FDEA201610123548.md): Skin · delaminated · Oct 12, 2016 · N10060 · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING INBD FLAP O/B HINGE PANEL 641CR DELAMINATED. REPAIRED THE DAMAGE IAW SRM 51-71-00 VOL II
- [SDR FDEA201610113544](https://openairdocs.org/sdr/FDEA201610113544.md): Skin · dented · Oct 11, 2016 · N10060 · Doug MD1010F · Elevator, Plate/Skin
  > RIGHT ELEVATOR LOWER SURFACE CREASED. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 55-10-00 FIG. 8 VOL. I
- [SDR FDEA201610043455](https://openairdocs.org/sdr/FDEA201610043455.md): Floorbeam · corroded · Oct 4, 2016 · N10060 · Doug MD1010F · Fuselage Main, Floor Beam
  > AFT CARGO BAY BS 1841 FLOORBEAM HAS SEVERAL AREAS WITH CORROSION. LBL TO RBL 18. REPAIRED IAW DWG AGA3874
- [SDR FDEA201610033647](https://openairdocs.org/sdr/FDEA201610033647.md): Acoustic Panel · cracked · Oct 3, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NR 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.
- [SDR FDEA201610033528](https://openairdocs.org/sdr/FDEA201610033528.md): Roller Tray · cracked · Oct 3, 2016 · N10060 · Doug MD1010F · Cargo Compartments
  > FWD CARGO ROLLER TRAY AT BS 920 DOOR ENTRY AREA CRACKED. REPLACED THE ROLLER TRAY IAW NDJ6030.
- [SDR FDEA201610023428](https://openairdocs.org/sdr/FDEA201610023428.md): Tee Fitting · cracked · Oct 2, 2016 · N10060 · Doug MD1010F · Fuselage Main, Bulkhead
  > RT 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.
- [SDR FDEA201610023427](https://openairdocs.org/sdr/FDEA201610023427.md): Tee Fitting · cracked · Oct 2, 2016 · N10060 · Doug MD1010F · Fuselage Main, Bulkhead
  > RT 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.
- [SDR FDEA201610023426](https://openairdocs.org/sdr/FDEA201610023426.md): Tee Fitting · cracked · Oct 2, 2016 · N10060 · Doug MD1010F · Fuselage Main, Bulkhead
  > LEFT BS 595 BULKHEAD TEE CAP AT LONGERON 39L HAS A.5 IN CRACK AT THE LWR FASTENER. REPAIRED IAW EA 8-5310-T0328709.
- [SDR FDEA201610013904](https://openairdocs.org/sdr/FDEA201610013904.md): Bolt · sheared · Oct 1, 2016 · N10060 · Doug MD1010F · Nacelle/Pylon, Main Frame
  > NR 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.

Next page: https://openairdocs.org/deregistered/N10060-2024-03-02/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 = 'N10060' AND deregistration_id = 'N10060-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N10060-2024-03-02/reports

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