# Service difficulty reports: N392FE, cancelled Jan 29, 2024

A list on [N392FE, cancelled Jan 29, 2024](https://openairdocs.org/deregistered/N392FE-2024-01-29.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 2 · 70 reports

- [SDR FDEA201412114107](https://openairdocs.org/sdr/FDEA201412114107.md): Battery Pack · failed · Dec 11, 2014 · N392FE · Doug MD1010F · Emergency Lighting
  > DURING SERVICE CHECK, FOUND EMERGENCY LIGHT BATTERY NR 1 LOW ALERT. REPLACED THE BATTERY PACK. OPS CHECKED GOOD.
- [SDR FDEA201408052076](https://openairdocs.org/sdr/FDEA201408052076.md): Skin · cracked · Aug 5, 2014 · N392FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING FIXED LE VI FOUND EVIDENCE OF CRACKS AT THE TAI. TELESCOPING DUCT CUT OUT TOP CORNERS COMPLIES WITH EA 8-5710-T0309830 P1 BY REPAIRING USING SRM 57-40-01 AS A REFERENCE.
- [SDR FDEA201403270594](https://openairdocs.org/sdr/FDEA201403270594.md): Lamp · inoperative · Mar 27, 2014 · N392FE · Doug MD1010F · Emergency Lighting
  > R1 DOOR SLIDE LIGHT WILL NOT TEST CORRECTLY. REPLACED LAMP IAW SMP. OPS NORMAL.
- [SDR FDEA201403190533](https://openairdocs.org/sdr/FDEA201403190533.md): Connector · loose · Mar 19, 2014 · N392FE · Doug MD1010F · Equipment/Furnishings Wiring
  > R1 DOOR LIGHT FOR SLIDE INOPERATIVE. SECURED ELECTRICAL CONNECTOR ON WIRE LEAD TO PRESS TO TEST SWITCH. PRESS TO TEST SYSTEM FOR BATTERY AND LIGHT FUNCTION NORMALLY IAW AMM 25-61-01-2.
- [SDR FDEA201311232855](https://openairdocs.org/sdr/FDEA201311232855.md): Bottle · low pressure · Nov 23, 2013 · N392FE · Doug MD1010F · Passenger/Crew Doors
  > RIGHT ENTRY DOOR PNEUMATIC BOTTLE PRESSURE 0. FOUND DOOR R1 HANDLE IN THE EMERGENCY POSITION. RESET DOOR HANDLE & SERVICED DOOR ASSIST BOTTLE IAW MD10-10 MM 52-11-07-2, OPERATIONS NORMAL.
- [SDR FDEA201307101522](https://openairdocs.org/sdr/FDEA201307101522.md): Fire Detector · false activation · Jul 10, 2013 · N392FE · Doug MD1010F · Fire Detection
  > THIRTY MINUTES AFTER TAKEOFF, RECEIVED A LEVEL 3 ALERT, LOWER CARGO FWD FIRE. DISCHARGED FIRE AGENT IAW PHASE 1 PROCEDEURES, RAN RED TABS. DIVERTED, CRASHED. FIRE RESCUE INSPECTED ACFT AND FOUND NO INDICATION OF FIRE. INSPECTED FWD LOWER CARGO BAY FOR ANY
- [SDR FDEA201303010480](https://openairdocs.org/sdr/FDEA201303010480.md): Windshield · failed · Mar 1, 2013 · N392FE · Doug MD1010F · Flight Compartment Windows
  > ON FINAL APPROACH, MODERATE RIM ICE ACCUMULATATED ON F/O WINDSHIELD, ALMOST NO ICE ON CAPT SIDE. WINDSHIELD A/I HAD BEEN ON FOR ABOUT 10 MIN ON LOW ON BOTH SIDES. HIGH WAS THEN SELECTED AND WITHIN 30, " F/O WINDSHIELD CRACKED." REPAIRED IAW AMM 56-11-00-2
- [SDR FDEA201301040012](https://openairdocs.org/sdr/FDEA201301040012.md): Relay · intermittent · Jan 4, 2013 · N392FE · Doug MD1010F · Pneumatic Indicating System
  > AIR MANIFOLD NR 3 FAILED LEVEL 3 ALERT WHEN ANTI-ICE SELECTED ON DURING DESCENT. PERFORMED TEST OF THE PNEUMATIC PRESSURE SW IAW EA 8-3622-114705, SWITCH OPS NORMAL, BUR FOUND FAILED. RELAY R2-5257 INTERMITTENT, REPLACED RELAY AND PERFORMED TESTS IAW FIM 3
- [SDR FDEA201301030011](https://openairdocs.org/sdr/FDEA201301030011.md): Relay · failed · Jan 3, 2013 · N392FE · Doug MD1010F · Pneumatic Indicating System
  > AIR MANIFOLD NR 3 FAILED LEVEL 3 ALERT WHEN ANTI-ICE SELECTED ON, DURING DESCENT. PERFORMED A GVI OF PNUEMATIC DUCTS AND VALVES IN WING AND PYLON AREA. PERFORMED PNEUMATIC DECAY TEST IAW AMM 36-00-01-5 WITH NO FAULTS. DURING SYS TESTS USING APU, FOUND THE MA
- [SDR FDEA201107152714](https://openairdocs.org/sdr/FDEA201107152714.md): Shaft · sheared · Jul 15, 2011 · N392FE · Doug MD1010F · Cabin Cooling System
  > NR1 ACM PACK RUNS ALMOST FULL HOT REGARDLESS OF RAM AIR DOOR AND PACK VALVE TRANSMITTER POSITIONS. REMOVED NR 1 ACM PACK, FOUND A BROKEN TURNBINE SHAFT. R & R AIR CYCLE MACHINE POSSITION NR 1.
- [SDR FDEA201107072608](https://openairdocs.org/sdr/FDEA201107072608.md): Spar Cap · cracked · Jul 7, 2011 · N392FE · Doug MD1010F · Wing Spar
  > RT WING REAR SPAR CAP HAS 2 HOLES WITH CRACK INDICATION. ACCOMPLISHED LIMITED REPAIR REF EA 8-5710-147784. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 24 MONTHS.
- [SDR FDEA201106132224](https://openairdocs.org/sdr/FDEA201106132224.md): Angle · corroded · Jun 13, 2011 · N392FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT AT STA 1841 FLOOR AFT FRAME ANGLE FOUND CORRODED FROM UNDERNEATH AT NUT PLATE HOLES FROM LONGERON 42L TO 42R. FABRICATED NEW ANGLE WITH 7075-0 IAW WITH SRM 53-00-01 AND DWG AGA3874. PART HEAT TREATED TO T6. INSTALLED NEW ANGLE AT STA 1
- [SDR FDEA201106112207](https://openairdocs.org/sdr/FDEA201106112207.md): Roller Tray · corroded · Jun 11, 2011 · N392FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > 4 ROLLER TRAYS HAVE CORROSION, CENTER PIT BETWEEN STA 1700 TO 1781 CLEANED SURFACE CORROSION ON 3 TRAYS IAW SRM 51-21-01, VOL III. FABRICATED ONE ROLLER TRAY IAW DWG AFJ 7001. INSTALLED NEW TRAY IAW DWG AFJ7001.
- [SDR FDEA201106112206](https://openairdocs.org/sdr/FDEA201106112206.md): Floorbeam · corroded · Jun 11, 2011 · N392FE · Doug MD1010F · Fuselage Main, Floor Beam
  > CTR CARGO, AFT WALL FLOORBEAM ANGLE CORRODED ON AFT SIDE (AS VIEWED FROM AFT CARGO). R & R LT FLOORBEAM ANGLE SECTION, REF AFA3871, CLEANED AND TREATED CTR AND RT FLOORBEAM ANGLE SECTIONS, REF SRM 51-21-01, VOL II, LT FLOOR SUPPORT ANGLE 13 CORRODED BEYOND R
- [SDR FDEA201106062129](https://openairdocs.org/sdr/FDEA201106062129.md): Support · corroded · Jun 6, 2011 · N392FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CENTER CARGO AFT WALL, CORROSION ON VERTICAL SUPPORT BEAM JUST RIGHT OF CTR AND JUST ABOVE FLOOR LINE. INSTALLED NEW VERTICAL SUPPORT BEAM AT STA 1781 IAW DWG AFA3225 AND SRM 51-35-01, VOL II.
- [SDR FDEA201006162031](https://openairdocs.org/sdr/FDEA201006162031.md): Relief Valve · leaking · Jun 16, 2010 · N392FE · Doug MD1010F · Hydraulic System, Main
  > ON CLIMBOUT, GOT HYD 3 ELEV OFF ALERT WITH DECREASING HYD 3 QTY. FOLLOW ON ALERTS HYD 3 OFF AND ON FINAL APPROACH BACK TO DEPARTURE GOT HYD 3 FAIL. LOST ALL HYD 3 QTY. ALTN GEAR EXTENSION USED. LDG WT 343,500LBS. AIRPORT CRASH FIRE RESCUE REPORTED SMOKE
- [SDR FDEA201004221292](https://openairdocs.org/sdr/FDEA201004221292.md): Pressure Switch · failed · Apr 22, 2010 · N392FE · Doug MD1010F · Pneumatic Indicating System
  > AT CRUISE ALTITUDE, RECEIVED LEVEL 3 MANIFOLD NR 1 FAIL ALERT. AIR SYS ISOLATED PROPERLY AND ALERT WENT AWAY. DIVERTED AND LANDED WITHOUT INCIDENT. R & R LT WING MANIFOLD FAILURE DETECTION PRESSURE SWITCH IAW. MM36-23-03-4. PERFORMED TEST IAW 36-23-03. R &
- [SDR FDEA201002210480](https://openairdocs.org/sdr/FDEA201002210480.md): Transducer · malfunctioned · Feb 21, 2010 · N392FE · Doug MD1010F · Landing Gear Position and Warning
  > ANTI-SKID R FAIL ON LANDING CYCLED AND NO CHANGE,ON 2ND. ATTEMPT TO LAND CAME ON AGAIN THEN WENT OUT, FLAPS 50 LANDING 4L CKED CFDS FOUND MSG. 324355, NR 7 WHEEL SPEED TRANSDUCER FAIL, NEEDS CPN 3215531, ORDERED PART. REMOVED NR 7 TRANSDUCER, INSPECTED CO
- [SDR FDEA201001100077](https://openairdocs.org/sdr/FDEA201001100077.md): Anti-Skid Sys · failed · Jan 10, 2010 · N392FE · Doug MD1010F · Brake Anti-Skid Section
  > LEVEL 2 ANTI-SKID R FAIL ON FINAL W/GEAR DOWN. ANTI-SKID WOULD NOT TEST W/GEAR UP AFTER GO AROUND. DID TEST AND FAIL ONCE GEAR DOWN. R & R NR 7 WHEEL SPEED TRANSDUCER IN REF TO AMM32-45-03-2, SPIN CKD GOOD AND NO FAULTS SHOWN ON ASCU. REACTIVATED NR 7 M
- [SDR FDEA201001090064](https://openairdocs.org/sdr/FDEA201001090064.md): Anti-Skid Sys · failed · Jan 9, 2010 · N392FE · Doug MD1010F · Brake Anti-Skid Section
  > GOT LEVEL 2 ANTI SKID FAIL ON FINAL. EXECUTED GA RAN QRH. UNEVENTFUL LANDING. HAD FIRE TRUCK LOOK AT BRAKES WITH INFARED. THEY STATED BRAKES WERE WARM NOT HOT. IAW RTS FOUND ASCU HAD INTERNAL FAULT. R & R ASCU IAW AMM 32-45-01-04. ACCOMPLISHED RTS IAW AMM
- [SDR FDEA201001050014](https://openairdocs.org/sdr/FDEA201001050014.md): Anti-Skid Sys · failed · Jan 5, 2010 · N392FE · Doug MD1010F · Brake Anti-Skid Section
  > WHILE CONDUCTING ILS APPROACH TO RWY 36R AT MEM RECEIVED LVL 2 ALERT ANTI SKID RT FAIL EXECUTED MISSED APPROCH, RAN QRH. FAILED MANUAL ANTI-SKID CHECK WERE VECTOR FOR ANOTHER APPROACH AND ANTI-SKID APPEARED TO WORK. REMOVED AND REPLACED ASCU IAW MM 32-45-0
- [SDR FDEA200907042475](https://openairdocs.org/sdr/FDEA200907042475.md): Fitting · cracked · Jul 4, 2009 · N392FE · Doug MD1010F · Leading Edge Devices
  > RIGHT WING NR 2 SLAT FOUND CRACKED AT INBOARD FITTING. REMOVED AND REPLACED RT WING NR 2 SLAT AND ADJUSTED IAW AMM 27-80-01-4.
- [SDR FDEA200906152113](https://openairdocs.org/sdr/FDEA200906152113.md): Web · cracked · Jun 15, 2009 · N392FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > N/R206- 5 IN CRACK ON UPPER WEB INBD SIDE NR 3 PYLON APPROX 12 IN. FROM AFT PYLON MOUNT. REMOVED UPPER WEB ATNR 3 PYLON REF SRM 51-00-01. FABRICATED NEW WEB REF DRAWING AUB7031. INSTALLED NEW WEB REF 51-00-01 VOL 1, E.O. 5-5410-7-4311 P2 AND EO 8-5410-7-4311 P
- [SDR FDEA200901290379](https://openairdocs.org/sdr/FDEA200901290379.md): Pressure Panel · cracked · Jan 29, 2009 · N392FE · Doug MD1010F · Fuselage Main, Bulkhead
  > LT MLG WHEEL WELL INBD WALL UPPER AFT CORNER HAS CRACK FROM STIFFENER GOING FWD TOWARD PREVIOUS REPAIR, VERIFIED AND MARKED USING ET, LOCATED ABOVE NR 1 HYD SYSTEM RESERVOIR COMPLIED WITH EA 8-5310-123830 TITLE, FUSELAGE-MAIN FRAME- KEEL STRUCTURE/UNDERWING BA
- [SDR 06FDEA1650](https://openairdocs.org/sdr/06FDEA1650.md): Skin · bulged · Apr 30, 2006 · N392FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FOUND CENTER PIT STA 1731 ABOVE L45R TORQUE BOX WEB (SILL AREA) SKIN BULGE AND SHEARED RIVET. ENTERED IN ERROR WRONG AIRCRAFT, NO NON-ROUTINE N00200 FOR AIRCRAFT N392FE.
- [SDR 06FDEA1245](https://openairdocs.org/sdr/06FDEA1245.md): Repair · unknown · Mar 27, 2006 · N392FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > RT FUSELAGE EXTERNAL REPAIR IS IN CRITICAL AREA OF PRIMARY STATIC PORT. REWORKED REPAIR IAW FEDX EA 8-5330-96383 FUSELAGE - SKIN AT FORWARD CARGO DOOR HAS REPAIR THAT WAS REMOVED - REWORK. MAJOR REPAIR.
- [SDR 06FDEA0535](https://openairdocs.org/sdr/06FDEA0535.md): Sensor · out of adjust · Feb 3, 2006 · N392FE · Doug DC1010F · Leading Edge Slat Position Indicating System
  > ON APPROACH TO KSMF AT FLAPS 22, SLAT EXTEND SELECTION OF FLAPS 35 CAUSE A SLAT DISAGREE. RAN QRH LANDED FLAPS 22/SLATEXT. FOUND SENSOR GAP BEYOND MAX LIMIT. ADJUST SENSORS L4A AND L4B. RETENSIONED LT WING O/B SLATS AND SAFETIED PER M/M 27-80-00-5-2 CLOSED
- [SDR 05FDEA00097](https://openairdocs.org/sdr/05FDEA00097.md): Computer · malfunctioned · Jan 15, 2005 · N392FE · Doug MD1010F · ATC Transponder System
  > DURING APPROACH TO RWY 35R AT MCO GOT TOO LOW TERRAIN WARNING. AT 400 FEET ON GLIDE SLOPE AND LOC EXECUTED MISSED APPROACH AND RETURNED TO SAME RWY. THE SAME THING HAPPENED ON SECOND APPROACH. TOO LOW TERRAIN, WARNING CONTINUED TO TOUCHDOWN. REMOVED & REPL
- [SDR 04FDEA02982](https://openairdocs.org/sdr/04FDEA02982.md): Fitting · worn · Oct 22, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > LT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND ALL HOLES HAVE EVIDENCE OF PITTING. REMOVED CORROSION AND PITTING FROM LUG AND BORES. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM57-20-00 VOL.I PAGE 16. INSTALLED BUSHINGS ON NR N01175.
- [SDR 04FDEA02981](https://openairdocs.org/sdr/04FDEA02981.md): Roller · worn · Oct 22, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > RT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND HOLES HAVE EVIDENCE OF PITTING. REMOVED PITTING AND CORROSION FROM LUG AND BORE. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM 57-20-00 VOL. I PAGE 16. BLENDED FLAT SPOTTED AREA IAW EA8-
- [SDR 04FDEA02952](https://openairdocs.org/sdr/04FDEA02952.md): Lavatory · not seated · Oct 18, 2004 · N392FE · Doug MD1010F · Lavatories
  > LAVATORY PAPER AND WASTE RECEPTACLE DOES NOT SEAL CORRECTLY. RESEALED LAVATORY PAPER AND WASTE RECEPTALE IAW MD10-10 SRM 51-41-01 VOL II AND EA 8-2540- 82478, SEALING OF FORWARD LAVATORY TRASH SHOUT.
- [SDR 04FDEA02951](https://openairdocs.org/sdr/04FDEA02951.md): Panel · misaligned · Oct 18, 2004 · N392FE · Doug MD1010F · Nacelle/Pylon, Main Frame
  > NR 1 PYLON PRECOOLER VENTILATOR PANEL ASSY PN AUB7054-501 FASTENER HOLES DO NOT ALIGN TO PYLON STRUCTURE. COMPLIED WITH EA 8-5480-81485 REV. A, NR 1 ENGINE VENTILATOR PANEL REPAIR.
- [SDR 04FDEA02950](https://openairdocs.org/sdr/04FDEA02950.md): Frame · cracked · Oct 18, 2004 · N392FE · Doug MD1010F · Engine Thrust Reverser
  > NR 2 ENGINE RT THRUST REVERSER TRAILING EDGE AFT FLANGE CRACKED APPROXIMATELY 6 INCHES FROM BOTTOM. COMPLIED WITH MFG EA 8-7830-81496
- [SDR 04FDEA02937](https://openairdocs.org/sdr/04FDEA02937.md): Hinge Fitting · corroded · Oct 15, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT HAND INBOARD FLAP PIVOT ATTACH POINT, OUTBOARD LUG FACE, OUTER SURFACE CORRODED. REMOVED CORROSION FROM LUG FACE, FOUND TO BE OUT OF LIMITS IAW DC10 CMM 57-52-01. COMPLIED WITH FEDEX EA 8-5750-81475, WINGS, RIGHT HAND INBOARD FLAP OUTBOARD HINGE PIVOT
- [SDR 04FDEA02914](https://openairdocs.org/sdr/04FDEA02914.md): Hinge · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > LT IB FLAP OB HINGE PIVOT BORE FACE PITTED AND GOUGED (AIRFRAME SIDE) LOCATION NR 3. REMOVED BUSHING, REMOVED CORROSION, AND COMPLIED WITH EA 8-5750-81473 REF NR N00295.
- [SDR 04FDEA02917](https://openairdocs.org/sdr/04FDEA02917.md): Fitting · cracked · Oct 11, 2004 · N392FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > CRACKED LONGERON END FITTING, AFT OF RIGHT HAND AIR CONDITIONING DOOR CUTOUT, LONGERON 35R, STA 535. REMOVED END FITTING IAW FEDEX SRM 51-35-01 VOLUME II PAGE 1, AREA ALODINED AND TREATED IAW FEDEX DC10 SRM 51-21-01 VOLUME II PAGE 1, RECEIVED NEW END FITTING
- [SDR 04FDEA02916](https://openairdocs.org/sdr/04FDEA02916.md): Hinge Fitting · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DACCMM 57-52-01, BORE FOUND OUT OF LIMITS, GENERATED RFTS, RECEIVED FEDEX EA8-5750-81492, REPAIRED BORE IAW DACCMM 57-52-01 AND FEDEX EA8-5750-81492. SEE NR N00
- [SDR 04FDEA02915](https://openairdocs.org/sdr/04FDEA02915.md): Support · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT HAND OUTBOARD FLAP INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE CORRODED (INBOARD SUPPORT). REMOVED CORROSION IAW DACCMM 57-52-02. ETCHED AND PEENED IAW DACCMM PERCENT &-52-02 AND 20-11-02. FABBED BUSHING IAW DACCMM 57-52-02 AND EA8-5750-81472. CA
- [SDR 04FDEA02913](https://openairdocs.org/sdr/04FDEA02913.md): Longeron · worn · Oct 11, 2004 · N392FE · Doug MD1010F · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE LEFT HAND CORE COWL UPPER CHAFE STRIP WORN. FABRICATED DOUBLER, FILLERS, AND STRAP FOR LONGERON REPAIR IAW FEDEX EA8-7110-81487. INSTALLED LONGERON REPAIR IAW DC10 SRM 51-35-01 VOLUME II. FABRICATED RUB STRIP IAW DAC DWG NSL6016. INSTALLED RUB
- [SDR 04FDEA02912](https://openairdocs.org/sdr/04FDEA02912.md): Support · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Wing, Control Surface Attach Fittings
  > LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCMM 57-44-07 AND FEDEX EA8-5750-81473. PRIMED LUGS IAW DC109 SRM 57-21-01 VOLUME II. BEGINNING BORE
- [SDR 04FDEA02911](https://openairdocs.org/sdr/04FDEA02911.md): Support · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW FEDEX EA8-5750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 SRM 51-21-01 VOLUME I
- [SDR 04FDEA02910](https://openairdocs.org/sdr/04FDEA02910.md): Support · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 3 HAS CORROSION IN BORE. REMOVED CORROSION IAW DACCMM 57-44-07. BEGINNING BORE 2.5850 INCH FINAL 2.626 INCH MATERIAL. REMOVED.041 INCH. FABRICATED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81473. ACCOMP
- [SDR 04FDEA02908](https://openairdocs.org/sdr/04FDEA02908.md): Support · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCMM 57-44-07 AND FEDEX EA8-5750- 81473. PRIMED LUGS IAW DC10 SRM 57-21-01 VOLUME I, BEGINNING BORE
- [SDR 04FDEA02907](https://openairdocs.org/sdr/04FDEA02907.md): Hinge Fitting · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT HAND INBOARD FLAP PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION BEGINNING BORE 1.1875 INCH FINAL 1.2583 INCH MATERIAL REMOVED.0708 INCH IAW DACCMM 57-52-01. FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475. PERFORMED MPI IAW
- [SDR 04FDEA02906](https://openairdocs.org/sdr/04FDEA02906.md): Support · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Wing Miscellaneous Structure
  > BORE CORRODED RIGHT WING INBOARD FLAP OUTBOARD HINGE LOWER SWIVEL BEARING. REMOVED CORROSION IAW DACCMM 57-44-07. ORIGINAL BORE 2.530 INCH FINAL 2.543 INCH MATERIAL LOSS.013 INCH. FABBED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81474. PERFORMED MPI IAW DP
- [SDR 04FDEA02905](https://openairdocs.org/sdr/04FDEA02905.md): Support · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Wing Miscellaneous Structure
  > RIGHT WING INBOARD FLAP OUTBOARD HINGE LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW EA8-8750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 SRM 51-21-01 VOLUME II. BEGIN
- [SDR 04FDEA02904](https://openairdocs.org/sdr/04FDEA02904.md): Skin · misrepaired · Oct 11, 2004 · N392FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > RIGHT HAND PRIMARY STATIC PORT FAILS RVSM INSPECTION FOR EXTERNAL DOUBLER MISMATCH RATIO IAW DC10 SRM 53-00-02 NOTE 2 (FIG 1 SHEET 2). REMOVED EXISTING FUSELAGE SKIN REPAIR ON FORWARD EDGE OF FORWARD CARGO DOOR CUTOUT DOUBLERS, FABRICATED NEW EXTERNAL DOUBLER
- [SDR 04FDEA02903](https://openairdocs.org/sdr/04FDEA02903.md): Hinge · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP INBOARD HINGE, LOCATION NR 4 BORE CORRODED. REMOVED CORROSION IAW DACCMM 57-44-08, INSPECTED IAW DACCMM 57-44-08 AND 20-11-02. PEENED IAW DACCMM 57-44-08 AND 20-11-01. PRIMED IAW DC10 SRM 51-21-01 VOL. II. FABBED BUSHING IAW DACCMM
- [SDR 04FDEA02902](https://openairdocs.org/sdr/04FDEA02902.md): Fitting · damaged · Oct 11, 2004 · N392FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT HAND INBD FLAP PIVOT POINT OUTBOARD BORE HAS GROOVE MARK. REMOVED CORROSION IAW DAC CMM 57-52-01. BEGINNING DIAMETER 1.1875 INCH FINAL 1.2552 INCH. FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475 MPI IAW DACCMM 5752-01 AND DPS 4.704 CAD P
- [SDR 04FDEA02901](https://openairdocs.org/sdr/04FDEA02901.md): Skin · corroded · Oct 11, 2004 · N392FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING SKIN LOWER SURFACE IS CORRODED, STATION XORS 799 APPROX 19 INCHES AFT OF FORWARD SPAR CAP. SKIN HAS SMALL AMOUNTS OF PITTING. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW EA 8-5710-81493. ORIGINAL MATERIAL THICKNESS IS.096 INCH, REMOVED.0

Next page: https://openairdocs.org/deregistered/N392FE-2024-01-29/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 = 'N392FE' AND deregistration_id = 'N392FE-2024-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N392FE-2024-01-29/reports

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