# Service difficulty reports: N310FE, cancelled Dec 16, 2009

A list on [N310FE, cancelled Dec 16, 2009](https://openairdocs.org/deregistered/N310FE-2009-12-16.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FDEA200810294607](https://openairdocs.org/sdr/FDEA200810294607.md): Handle · stuck · Oct 29, 2008 · N310FE · Doug DC1030F · Landing Gear Selector
  > ON DEPARTURE FROM MEM GEAR HANDLE WOULD NOT MOVE TO UP POSITION RAN QRH PROCEDURE FOR GEAR HANDLE, WILL NOT MOVE TO UP POSITION UNABLE TO RAISE GEAR HANDLE RETURNED TO MEM.
- [SDR 08FDEA04607](https://openairdocs.org/sdr/08FDEA04607.md): Handle · malfunctioned · Oct 29, 2008 · N310FE · Doug DC1030F · Landing Gear Selector
  > ON DEPARTURE FROM MEM, GEAR HANDLE WOULD NOT MOVE TO UP POSITION. RAN QRH PROCEDURE FOR GEAR HANDLE WILL NOT MOVE TO UP POSITION UNABLE TO RAISE GEAR HANDLE, RETURNED TO MEM.
- [SDR 08FDEA04373](https://openairdocs.org/sdr/08FDEA04373.md): Sense Line · leaking · Oct 15, 2008 · N310FE · Doug DC1030F · Pneumatic Indicating System
  > PNEU SUPPLY RED FAIL LIGHT ILLUMLINATED. PRESS GAUGE SYS NR 2 VERY HIGH, 30 PSI WOULD NOT GO DOWN WITH THROTTLE TO IDLE, SUPPLY PNEU SWITCH OFF, FINALLY PSI WENT TO 20 PSI. FOUND LEAKS ON LINE GOING TO FAN AIR VALVE. REMOVED AND REPLACED SENSE LINE PER SM
- [SDR 07FDEA01379](https://openairdocs.org/sdr/07FDEA01379.md): Handle · dirty · Apr 8, 2007 · N310FE · Doug DC1030 · Landing Gear Selector
  > PUT GEAR DOWN AND HAD 4 RED LIGHTS, PUSHED ANTI-SKID TEST AND ANTI-SKID LIGHTS REMAINED BLANK.RAISED GEA R AND LOWERED GOT 4 GREEN AND ANTI-SKID TESTED.SUSPR CT THE SWITCH WHEN THE GEAR HANDLE IS PUSHED IN, DURING PREFLT CHECKS IT WAS STICKY. JACKED ACFT AN
- [SDR 06FDEA04288](https://openairdocs.org/sdr/06FDEA04288.md): Duct · ruptured · Dec 20, 2006 · N310FE · Doug DC1030F · Pneumatic Distribution System
  > T/O AT SJC NR 2 THROTTLE MUCH FURTHER FWD THAN 1 AND 3 EGT NR 2 CREEPING UP, MAX TEMP = 880' C PULLED NR 2 THROTTLE BACK EVEN W/ 1 AND 3 GOT FIRE WARN, THROTTLE IDLE. SHUT DOWN ENGINE, FIRED BOTTLE NR 1 AS A PRECAUTION. DIVERT TO KOAK. DURING T/O N2 FOR AL
- [SDR 06FDEA2264](https://openairdocs.org/sdr/06FDEA2264.md): Hose · torn · Jun 10, 2006 · N310FE · Doug DC1030 · Pneumatic Distribution System
  > THE MANIFOLD FAILURE NR 1 & 2 LIGHTS ILLUMINATED. T/S PER DC-10 TAFI 36-23-00 FAULT CODE BD AND BE. THE 1 & 2 MANIFOLD FAIL LIGHTS WOULD ILLUMINATE WITH NO MANIFOLD PRESS. FOUND LOOPS 1A D1-44D AND 1B D1-38D SHORTED. REMOVED AND REPLACED LOOPS IAW DC-10-30
- [SDR 05FDEA03964](https://openairdocs.org/sdr/05FDEA03964.md): Duct · chafed · Nov 26, 2005 · N310FE · Doug DC1030F · Turbine Engine Reduction Gear
  > NR 1 ENG HIGH PRESSURE CONTROL VALVE CHAFING INTO 7TH STAGE AIR PRESSURE TURBINE CONTROL LINE. REMOVED 7TH STAGE COOLING TUBE, PER DC10-30 MM 75-22-00-02. REPAIRED DUCT PER EM 72-09-03. REINSTALLED DUCT AND HIGH PRESSURE VALVE. PERFORMED OPS AND LEAK CHECK
- [SDR 05FDEA03963](https://openairdocs.org/sdr/05FDEA03963.md): Pulley Bracket · chafed · Nov 26, 2005 · N310FE · Doug DC1030 · Fuselage Miscellaneous Structure
  > PILOTS AILERON CONTROL CABLE RUN NR 1 CHAFED INTO PULLEY BRACKET AT FS 395 LBL 30, 8 INCHES FROM BOTTOM FLOOR. PULLEY BRACKET REMOVED AND REPLACED IAW DC10-30 SRM 51-31-01 VOL 11. AILERON RIG PINS P-67 AND P-70 VERIFIED GOOD AND AILERON MECHANICAL TEST GOOD
- [SDR 05FDEA03928](https://openairdocs.org/sdr/05FDEA03928.md): Frame · cracked · Nov 21, 2005 · N310FE · Doug DC1030F · Engine Air Intake System
  > NR 1 ENG NOSE INLET COWL INTERIOR AFT BULKHEAD CHORD ANGLE IS CRACK AT 7 O`CLOCK POSITION CAN BE VIEWED FROM OUTBOARD SIDE. REMOVED AND REPAIRED CRACKED CHORD ANGLE IAW DC10 SRM 54-11-00 FIG 1C VOL 1. N/R N00405, W/O N/R 00030375.
- [SDR 05FDEA03929](https://openairdocs.org/sdr/05FDEA03929.md): Frame · cracked · Nov 21, 2005 · N310FE · Doug DC1030 · Nacelle/Pylon, Main Frame
  > NR 1 ENG NOSE INLET COWL INTERIOR AFT BULKHEAD CHORD ANGLE IS CRACK AT 7 O`CLOCK POSITION CAN BE VIEWED FROM OUTBOARED SIDE. REMOVED AND REPAIRED CRACKED CHORD ANGLE IAW DC10 SRM 54-11-00, FIG 1C VOL 1. N/R # N00405, W/O NR 00030375.
- [SDR 05FDEA03833](https://openairdocs.org/sdr/05FDEA03833.md): Floor Panel · corroded · Nov 16, 2005 · N310FE · Doug DC1030 · Fuselage Floor Panel
  > CENTER LOWER CARGO COMPT FLOOR PNL 183ZF HAS BROKE AND CORRODED INSERTS STA 1781 TO 1821 RBL 30 TO37. REMOVED AND REPLACED INSERTS IAW FEDEX DWG SRA 25-005 REV E.
- [SDR 05FDEA03832](https://openairdocs.org/sdr/05FDEA03832.md): Support · cracked · Nov 16, 2005 · N310FE · Doug DC1030 · Fuselage Miscellaneous Structure
  > FLOOR PANEL SUPPORTS AT STA 999 AND 1019 RBL 45 ARE CRACKED (2 EA). REMOVED, FABRICATED NEW FLOOR SUPPORT IAW DAC DRAWING NR ACA3763 REV H AND FEDEX GMM 7-0-1000, SEE FEDEX NONROUTINE N00734 OF WORK ORDER NR 0003075.
- [SDR 05FDEA03824](https://openairdocs.org/sdr/05FDEA03824.md): Support Angle · cracked · Nov 15, 2005 · N310FE · Doug DC1030 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENG NOSE COWL AFT SIDE LOWER SUPPORT WEB ANGLE FOR STARTER VALVE WAS CRACKED. REMOVED CRACK SUPPORT ANGLE FROM NR 1 ENGINE AFT SIDE OF AFT BULKHEAD NOSE COWL IAW DC10 SRM 51-31-01 VOL 11. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW DC10 SRM 51-31-01 VOL 1
- [SDR 05FDEA03811](https://openairdocs.org/sdr/05FDEA03811.md): Angle · cracked · Nov 14, 2005 · N310FE · Doug DC1030 · Fuselage Miscellaneous Structure
  > CTR CARGO COMPT ANGLE CRACKED AND BENT AT TOP AFT CORNER OF DOOR CUT-OUT FS 1781 LONG 29R. REMOVED ANGLE IAW DC10 SRM 51-35-01 VOL 11. MATERIAL ID FOUND TO BE 2024-T3 IAW ASTME 1476.050 IAW CALIPER NR E110484B. FAB`D AND PART MARKED IAW FED EX GMM 7-0-1001
- [SDR 05FDEA03768](https://openairdocs.org/sdr/05FDEA03768.md): Spar · cracked · Nov 11, 2005 · N310FE · Doug DC1030F · Wing Spar
  > RT WING, TRAILING EDGE HAS A TWO INCH LONG CRACK IN FITTING AT XORS, 14 INCHES AFT OF INNER REAR SPAR. REMOVED AND REPLACED SUPPORT FITTING ARCO472-42, ( PO# 509448.1) IAW DC10-30 SRM 51-33-01 VOLII. TIMCO MECHANIC 7921, QC INSPECTOR #QC35.
- [SDR 05FDEA03729](https://openairdocs.org/sdr/05FDEA03729.md): Skin · dented · Nov 9, 2005 · N310FE · Doug DC1030 · Leading Edge Devices
  > RT WING O/B FLAP LOWER O/B SURFACES HAS DENTS. FOUND DENTS AT X0F 775-781 TO BE WITHIN ALLOWABLE LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL 1. FOUND DENT AT X0F 783-787 TO BE OUT OF LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL1. REMOVED DAMAGE AND INSTALLED REPAIR
- [SDR 05FDEA03728](https://openairdocs.org/sdr/05FDEA03728.md): Skin · dented · Nov 9, 2005 · N310FE · Doug DC1030 · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP HAS DENTS 4 PLACES. DENTS AT XOF657, 639, AND 611 FOUND TO BE WITHIN LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL I. REPAIRED DENT AT XOF 516 IAW DC10 SRM 57-10-00 FIG 85 VOL I. SEE FEDEX NONROUTINE NR N00229 OF WORK ORDER 0030375.
- [SDR 05FDEA03722](https://openairdocs.org/sdr/05FDEA03722.md): Seat Track · worn · Nov 8, 2005 · N310FE · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STA 938 RBL 47.5 SEAT TRACK WORN, BLENDED AREA IAW DC10 SRM 53-70-00 VOL1 AREA HAS 50 PERCENT MAT'L LOSS AREA IS OUT OF LIMITS. MAT'L ID FOR NEW SEAT TRACK SECTION 54929150-1200 PO NR 502938.1 IAW DC10 SRM 53-42-01 VOL II. FABRICATED SEAT TRACK SE
- [SDR 05FDEA03720](https://openairdocs.org/sdr/05FDEA03720.md): Angle · cracked · Nov 8, 2005 · N310FE · Doug DC1030 · Cargo/Baggage Doors
  > FOUND FWD LOWER CARGO DOOR FRAME AT FWD HINGE POINT ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW DC-10 SRM 51-33-01 VOL II MATERIAL ID 2024-T3.040 BOEING DWG ADA 7118, PO 504475.2 FABED IAW DWG ADA 7118 PART MARKED IAW FEDEX GMM 7-0-1000.
- [SDR 05FDEA03717](https://openairdocs.org/sdr/05FDEA03717.md): Skin · dented · Nov 8, 2005 · N310FE · Doug DC1030 · Trailing Edge Flaps
  > LEFT WING INBD FLAP LOWER SKIN HAS SMALL DENTS. CHECKED DENT LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL I. FOUND TWO DENTS OUT OF LIMITS. REPAIRED DENTS AT XIFH 230-231 AND XIFH 278-280 IAW DC10 SRM 57-10-00 FIG 85 VOLI.
- [SDR 05FDEA03613](https://openairdocs.org/sdr/05FDEA03613.md): Skin · dented · Nov 3, 2005 · N310FE · Doug DC1030F · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP HAS SPEED TAPE (LINE REPAIR) AFT OF NR 7 TIRE. REMOVED TEMP REPAIR AND REPAIRED SKIN IAW DC10 SRM 57-10-00 VOL I AND FEDEX EA 8-5750-91110 PART 3. P3 MOD TYPE T MOD REV NO A PS P3. EA IS ATTACHED TO WORK CARD 57501429, WORK ORDER 000
- [SDR 04FDEA00884](https://openairdocs.org/sdr/04FDEA00884.md): Skin · corroded · Apr 8, 2004 · N310FE · Doug DC1030 · Wing, Center Box
  > EXFOLIATING CORROSION ON TOP OF CENTER WING AT STA 1331, LBL 97.0 ON AN AREA OF APPROXIMATELY 6 X 8 INCH. REMOVED ALL EVIDENCE OF CORROSION. INSTALLED FILLERS AND DOUBLERS AS PER EA 8-5730-74212-WING UPPER AFT SKIN PANEL, CENTER BOX-CORROSION.
- [SDR 04FDEA00414](https://openairdocs.org/sdr/04FDEA00414.md): Support · damaged · Feb 17, 2004 · N310FE · Doug DC1030 · Fuselage Miscellaneous Structure
  > STRUCTURE DAMAGE TO FORWARD SHUTTLE LOAD BAR TRANSMISSION SUPPORT AND ATTACHING FLOORBEAM STRUCTURE AT FUS. STA 879. REPAIRED LOWER FLOOR BEAM STA.879 AS PER SRM53-60-01 FIGUARE 3 AND AND EA 8-5310- 71818.REF WORD CARD SEQ0005.
- [SDR 03FDEA02070](https://openairdocs.org/sdr/03FDEA02070.md): Engine · failed · Dec 5, 2003 · N310FE · Doug DC1030 · Engine (Turbine/Turboprop)
  > AT LEVEL OFF FL 330 EXPERIENCED HARD THUMP FOLLOWED BY GRINDING VIBRATION. IMMEDIATELY SHUT NR 1 DOWN. FOLLOWED QRH PROCEDURES, LANDED KPHX. PHX U C/W MD10-30 WORK CARD 71T0101-1, AND 71T0701-1.
- [SDR 02FDEA00137](https://openairdocs.org/sdr/02FDEA00137.md): Door · cracked · Feb 20, 2002 · N310FE · Doug DC1030F · Landing Gear Doors
  > ON GEAR RETRACT RT MLG IND UNSAFE ON BOTH PANELS. REMOVED AND REPLACED MAIN GEAR DOOR PER AMM 32-14-01-2.
- [SDR 01FDEA00811](https://openairdocs.org/sdr/01FDEA00811.md): Pressure Panel · corroded · Sep 5, 2001 · N310FE · Doug DC1030F · Fuselage Main, Bulkhead
  > CTR WHEEL WELL, LT SIDEWALL, LWR FWD CORNER, CORROSION UNDER SEALANT, AROUND ACCESS PNL.
- [SDR 01FDEA00162](https://openairdocs.org/sdr/01FDEA00162.md): Pump · failed · Feb 25, 2001 · N310FE · Doug DC1030F · Fuel Boost Pump
  > LOST NR 2 LT AND NR 2 RT AND NR 3 AFT TANK PUMPS. REMOVED AND REPLACED LT AFT FUEL BOOST PUMP. OPS CK NORM PER MM. CK WIRING TO ALL 3 PUMPS NO FAULT FOUND. ALL PUMPS OPS NORMAL.
- [SDR 01FDEA00144](https://openairdocs.org/sdr/01FDEA00144.md): Handle · missing · Feb 19, 2001 · N310FE · Doug DC1030F · Cargo/Baggage Doors
  > ON WALK-AROUND FOUND CTR LWR CARGO VENT PANEL HANDLE ACCESS MISSING. INSTALLED VENT PANEL HANDLE ACCESS DOOR PER STANDARD PRACTICE, OPS CK GOOD.
- [SDR 99FDEA00494](https://openairdocs.org/sdr/99FDEA00494.md): Warning Light · illuminated · Dec 1, 1999 · N310FE · Doug DC1030F · Airfoil Anti/De-ice System
  > NR 3 PNEUMATIC FAIL LIGHT ILLUM. COMPLETED RED TABS.
- [SDR 99FDEA00388](https://openairdocs.org/sdr/99FDEA00388.md): Seat Track · cracked · Sep 14, 1999 · N310FE · Doug DC1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK UPPER CARGO, SEAT TRACK CRACKED AT BS 635 X=27.5-242. UPPER CARGO SEAT CRACK AT BS Y=755 INTERSECTING X=8.5. *S/D* REPAIRED MDUC PER SRM 53-70-00 VOL 1-242 & UCST PER SRM 53-70-00 VOL 1-243.
- [SDR 99FDEA00384](https://openairdocs.org/sdr/99FDEA00384.md): Skin · cracked · Sep 10, 1999 · N310FE · Doug DC1030F · Wing, Plate/Skin
  > RT WING LOWER SURFACE OF LEADING EDGE ALONG XORS 402 FOUND WITH 2 INCH CRACK. *S/D* REPAIR CARRIED OUT PER SRM 57-10-00 FIG 68 VOL 1.
- [SDR 99FDEA00369](https://openairdocs.org/sdr/99FDEA00369.md): Tr Cowl · departed · Sep 6, 1999 · N310FE · Doug DC1030F · Engine Thrust Reverser
  > NR 2 ENGINE THRUST REVERSER TRANSLATING COWL DEPARTED THE A/C ON LANDING. *S/D* REMOVED AND REPLACED NR 2 RT T/R FAN IAW MM 78-32-11-2.
- [SDR 98FDEA00514](https://openairdocs.org/sdr/98FDEA00514.md): Light · inoperative · Aug 16, 1998 · N310FE · Doug DC1030F · Door Warning System
  > IN CRUISE FLT LEVEL 370, AIR COND DOOR LIGHT ILLUM. CONSULT RED TABS, RETURNED TO ANC. DOOR LIGHT WENT OUT AT 6.5 PSI. BEG TO BLINK WHEN INCREASE PSI AT 7.0 PSI. A/C RELEASED PER MEL 52-4D. A/C COND DOOR CAUTION LIGHT INOP. C/W MSP 52-4C, DOORS ARE VERIF
- [SDR 97FDEA00234](https://openairdocs.org/sdr/97FDEA00234.md): Fire Bottle · malfunction · Apr 16, 1997 · N310FE · Doug DC1030F · Extinguishing System
  > AFTER TAKEOFF, AGENT LOW LIGHT ILLUMINATED ON NR 2 ENGINE. FLIGHT RETURNED TO SFS AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE, NR 1 FIRE BOTTLE AND SQUIBS.
- [SDR 95FDEA01535](https://openairdocs.org/sdr/95FDEA01535.md): Prox Sensor · defective · Oct 10, 1995 · N310FE · Doug DC1030F · Landing Gear Position and Warning
  > LT MAIN IND UNSAFE, BOTH PANELS WITH GEAR HANDLE UP. INITIALLY GEAR WENT UP SAFE, BUT AFTER ABOUT 5 SECONDS THE RED LIGHT CAME BACK ON, THIS OCCURRED ON TWO OCCASIONS. FOUND LT/MLG DOWN LOCK SENSOR WIRES DEFECTIVE. REMOVED AND REPLACED POSITION PROXIMITY SE
- [SDR 95FDEA01281](https://openairdocs.org/sdr/95FDEA01281.md): Skin · lightning strike · Sep 2, 1995 · N310FE · Doug DC1030F · Rudder, Tab Structure
  > LIGHTNING STRIKE, TOP OF UPPER RUDDER TAB RT SIDE, APPROX.25 INCH HOLE BURNED THROUGH ALUMINUM SKIN. FABRICATED DOUBLER PER SRM 55-00-01, WEIGHT CHANGE PLUS 1.502. RESTAMPED PLACARD TO ACTUAL WT OF RUDDER AS REQ SRM 55-40-02, PRIMED AND PAINTED PER SRM 51-2
- [SDR 95FDEA01280](https://openairdocs.org/sdr/95FDEA01280.md): Fitting · loose · Aug 24, 1995 · N310FE · Doug DC1030F · Trailing Edge Flaps
  > RT WING O/B FLAP I/B SUPPORT FITTING TO REAR SPAR IS SUSPECTED LOOSE, MEASURED GAP 0.003. REMOVED O/B FLAP AND INSPECTED SUPT FITTING HOLES FOR CRACKS, NO DEFECTS NOTED. INSTALLED NEW STUDS AND PLI WASHERS AS PER MM 20-20-01 PG 202. REINSTALLED FLAP, FITTIN
- [SDR 95FDEA01279](https://openairdocs.org/sdr/95FDEA01279.md): Fitting · worn · Aug 24, 1995 · N310FE · Doug DC1030F · Elevator Structure
  > RT DETACHABLE ELEVATOR'S BAYONET LATCHES ARE LOOSE, WORN FITTINGS C/W S/B 55-9 AND EA NR 8-5520-25164. REPLACED FITTINGS AND LATCHES, OPENED AND CLOSED SKIN AND SEAL EDGES. ELEV OPS CHECK OK.
- [SDR 95FDEA01278](https://openairdocs.org/sdr/95FDEA01278.md): Fitting · worn · Aug 24, 1995 · N310FE · Doug DC1030F · Elevator Structure
  > LT DETACHABLE ELEVATOR, AFT BAYONET LATCH ASSY LOOSE IN FITTING, WORN C/W SB 55-9 AND EA NR 8-5520-25165. OPEN SKIN, REPLACED FITTINGS AND LATCHES. SKIN AND PANELS OPS CHECK OK.
- [SDR 95FDEA01277](https://openairdocs.org/sdr/95FDEA01277.md): Frame · cracked · Aug 22, 1995 · N310FE · Doug DC1030F · Landing Gear Doors
  > LT CENTER GEAR DOOR, 2 INCH CRACK AT FWD I/B FRAME. REMOVED AND REPLACED DAMAGED FRAME AS PER SRM 51-00-00 PG 2 ITEM C.
- [SDR 95FDEA01276](https://openairdocs.org/sdr/95FDEA01276.md): Frame · cracked · Aug 22, 1995 · N310FE · Doug DC1030F · Landing Gear Doors
  > RT CENTER GEAR DOOR, 2 INCH CRACK AT FWD I/B FRAME. REMOVED AND REPLACED DAMAGED FRAME AS PER SRM 51-00-00 PG 2 ITEM C.

## 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 = 'N310FE' AND deregistration_id = 'N310FE-2009-12-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N310FE-2009-12-16/reports

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