# Service difficulty reports: N579FE, cancelled Mar 2, 2024 A list on [N579FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N579FE-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 6 · 254 reports - [SDR FDEA201311192828](https://openairdocs.org/sdr/FDEA201311192828.md): Sensor · failed · Nov 19, 2013 · N579FE · Doug MD11F · Leading Edge Slat Position Indicating System > UPON CONFIGURATION AT 15 DEG FLAPS, LEVEL 2 SLAT DISAGREE ILLUMINATED, GO AROUND. RAN CHECKLIST ON EXTENDED DOWNWIND. DURING GO AROUND THERE WAS SOME FEEL THAT CONFIGURATION WAS OFF. LANDED SLAT STOW FLAPS 28 DEGREES AT 185KTS & MAX BRAKES. RAN SLATS VER - [SDR FDEA201308011738](https://openairdocs.org/sdr/FDEA201308011738.md): Wheel · failed · Aug 1, 2013 · N579FE · Doug MD11F · Wheel/Ski/Float > LEVEL 2 TIRE FAIL ON LANDING ROLL, R & R NR 10 MAIN WHEEL ASSY IAW 32-41-01-4 UP TO STEP 5F(6). - [SDR FDEA201307201601](https://openairdocs.org/sdr/FDEA201307201601.md): Switch · failed · Jul 20, 2013 · N579FE · Doug MD11F · Passenger/Crew Doors > SLIDE PRESSURE LIGHT IN L1 DOOR WAS INOPERATIVE, REPLACED LIGHT SWITCH ASSY IAW MM 25-61-04-4. OPS CHECKED NORMAL. - [SDR FDEA201304080743](https://openairdocs.org/sdr/FDEA201304080743.md): Transmitter · malfunctioned · Apr 8, 2013 · N579FE · Doug MD11F · Fuel Indicating System > PASSING THRU FL 260 RECEIVED A LEVEL 2 FUEL QTY/USED CHECK. FUEL USED ON ALL THREE ENGINES TOTALED WITH FUEL ONBOARD TOTALED 58.8 VICE FOB OF 56.4 AT TAKEOFF. RAN CHECK LIST AND DECIDED TO LEAVE ALL THREE ENG RUNNING. DURING DESCENT FUEL USED ON ENGINE 1 - [SDR FDEA201212084268](https://openairdocs.org/sdr/FDEA201212084268.md): Skin · loose · Dec 8, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > LEFT WING INBD FLAP UPPER SURFACE AT XIFH= 171 RIVETS FOUND LOOSE. REPAIRED IAW SRM 57-50-01 FIGURE 201 REPAIR 4 REVISION 51 AND EA 1-5750-163534 STEP 5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201212074267](https://openairdocs.org/sdr/FDEA201212074267.md): Bulkhead · misrepaired · Dec 7, 2012 · N579FE · Doug MD11F · Fuselage Main, Bulkhead > NLG HORIZONTAL PRESSURE PANEL, LT SIDE, BS 495 TO 515, "X"=30 TO "X"=39 MISREPAIRED. REPAIRED IAW EA 1-5310-163550. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201212074266](https://openairdocs.org/sdr/FDEA201212074266.md): Bulkhead · misrepaired · Dec 7, 2012 · N579FE · Doug MD11F · Fuselage Main, Bulkhead > NLG HORIZONTAL PRESSURE PANEL, LT SIDE, AT BS 495 TO 515, "X"=42 TO "X"=47 MISREPAIRED. REPAIRED IAW EA 1-5310-163550. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201212074265](https://openairdocs.org/sdr/FDEA201212074265.md): Floorbeam · misrepaired · Dec 7, 2012 · N579FE · Doug MD11F · Fuselage Main, Structure > FLOORBEAM LOWER FLANGE AT BS 5-53 MISREPAIRED. REPAIRED IAW EA 1-5310-163551. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201212074264](https://openairdocs.org/sdr/FDEA201212074264.md): Hinge Bracket · corroded · Dec 7, 2012 · N579FE · Doug MD11F · Wing, Control Surface Attach Fittings > RT WING, OTBD FLAP, INBD FORWARD HINGE BRACKET, LOWER MOUNT INBD BORE FOUND CORRODED. REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER: 0.705", FINAL HOLE DIAMETER: 0.709", MAXIMUM HOLE: 0.709". REPAIR BUSHING FABR - [SDR FDEA201211304215](https://openairdocs.org/sdr/FDEA201211304215.md): Hinge Bracket · corroded · Nov 30, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE LOAD FITTING UPPER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. EXISTING THICKNESS: 0.452", MATERIAL REMOVED: 0.004", REAMINING THICKNESS: 0.448" FOUND ACCEPTABLE PER EA 1-5750-162 - [SDR FDEA201211304216](https://openairdocs.org/sdr/FDEA201211304216.md): Hinge Bracket · corroded · Nov 30, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > LT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING LOWER BORE SURFACE CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. EXISTING THICKNESS: 0.452", MATERIAL REMOVED: 0.004", REAMINING THICKNESS: 0.448" FOUND ACCEPTABLE PER EA 1-5750-162399 P - [SDR FDEA201211294198](https://openairdocs.org/sdr/FDEA201211294198.md): Skin · loose · Nov 29, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING INBD FLAP UPPER SURFACE RIVETS XIFH 261 FOUND LOOSE. REMOVED AND REPAIR ACCOMPLISHED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115. - [SDR FDEA201211294201](https://openairdocs.org/sdr/FDEA201211294201.md): Stop Fitting · cracked · Nov 29, 2012 · N579FE · Doug MD11F · Fuselage Main, Structure > ON REMOVAL OF R1 MED DUST COVER NR 3 DOOR BEAM AFT STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 51 AND EA 1-5210-163538. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211294200](https://openairdocs.org/sdr/FDEA201211294200.md): Stop Fitting · cracked · Nov 29, 2012 · N579FE · Doug MD11F · Fuselage Main, Structure > ON REMOVAL OF R1 MED DUST COVER NR 2 DOOR BEAM AFT STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 51 AND EA 1-5210-163538. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211284192](https://openairdocs.org/sdr/FDEA201211284192.md): Frame · cracked · Nov 28, 2012 · N579FE · Doug MD11F · Engine Thrust Reverser > NR 1 ENGINE THRUST REVERSER AFT CASCADE SUPPORT FRAME AT POSITION 6 FOUND CRACKED AT NUTPLATE AREA. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER SUPPORT FRAME AS PER EA 1-7830-163531. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115. - [SDR FDEA201211284189](https://openairdocs.org/sdr/FDEA201211284189.md): Skin · loose · Nov 28, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING INBD FLAP UPPER SURFACE AT "XIFH" = 269 FOUND LOOSE RIVETS. REMOVED AND REPAIRED ACCOMPLISHED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115. - [SDR FDEA201211264180](https://openairdocs.org/sdr/FDEA201211264180.md): Skin · corroded · Nov 26, 2012 · N579FE · Doug MD11F · Fuselage Main, Plate/Skin > AFT ACCESSORY COMPARTMENT, FUSELAGE RT SIDE, SKIN AT STATION 2163 TO 2140, BETWEEN LONGERON 33 RIGHT AND 35 RIGHT, FOUND SURFACE CORROSION ON INTERIOR AREA COMMON TO EXISTING EXTERIOR REPAIR DOUBLER. REPAIRED IAW SRM 51-21-01 REVISION 51. FOUND EXCEEDED L - [SDR FDEA201211264158](https://openairdocs.org/sdr/FDEA201211264158.md): Seat Track · corroded · Nov 26, 2012 · N579FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > BS 1385, "X"= 8.5. SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201211264157](https://openairdocs.org/sdr/FDEA201211264157.md): Seat Track · corroded · Nov 26, 2012 · N579FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > BS 1451, "X"= 8.5, SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53- 00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201211264160](https://openairdocs.org/sdr/FDEA201211264160.md): Seat Track · corroded · Nov 26, 2012 · N579FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > BS 1641, "X"=-8.5, SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR AS IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201211264159](https://openairdocs.org/sdr/FDEA201211264159.md): Seat Track · corroded · Nov 26, 2012 · N579FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings > BS 1884 TO 1887, "X"=-8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201211234132](https://openairdocs.org/sdr/FDEA201211234132.md): Web · canning · Nov 23, 2012 · N579FE · Doug MD11F · Fuselage Miscellaneous Structure > CENTER LANDING GEAR LT KEEL WEB AT BS 1431 OIL CANNING FOUND EXCEED SRM ALLOWABLE LIMITS. REPAIRED IAW EA 1-5310-163532. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201211224122](https://openairdocs.org/sdr/FDEA201211224122.md): Skin · misrepaired · Nov 22, 2012 · N579FE · Doug MD11F · Fuselage Main, Plate/Skin > SKIN MISREPAIRED AT BS 1846, LONGEON 42 TO 44 RIGHT. REPAIRED IAW EA 1-5330-163536. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211214115](https://openairdocs.org/sdr/FDEA201211214115.md): Web · cracked · Nov 21, 2012 · N579FE · Doug MD11F · Fuselage Miscellaneous Structure > RT OBSERVER SEAT, LOWER FLOOR WEB FOUND EDGE CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-51, REPAIR 1, FIGURE 202, REVISION 51. REPAIR PARTS INSTALLED IAW SRM 51-35-01, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 115. - [SDR FDEA201211214107](https://openairdocs.org/sdr/FDEA201211214107.md): Frame · cracked · Nov 21, 2012 · N579FE · Doug MD11F · Fuselage Main, Frame > FRAME END CAP AT BS 555, NEAR LONGERON 32R, IN AIR CONDITION PACK NR 3 COMPARTMENT, FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-35- 01, REVISION 51.. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 115. - [SDR FDEA201211194084](https://openairdocs.org/sdr/FDEA201211194084.md): Hinge Bracket · damaged · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND EXCEEDED LIMITS AFTER BUSHING REMOVED. REPAIRED PER EA 1-5750-75980 REVISION A PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211194097](https://openairdocs.org/sdr/FDEA201211194097.md): Skin · loose · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > LEFT WING INBD FLAP UPPER SURFACE RIVETS FOUND LOOSE. REPAIRED IAW SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163534, STEP 4, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211194096](https://openairdocs.org/sdr/FDEA201211194096.md): Skin · loose · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING INBD FLAP UPPER SURFACE RIVETS FOUND LOOSE. REMOVED AND REPAIRED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115. - [SDR FDEA201211194095](https://openairdocs.org/sdr/FDEA201211194095.md): Hinge Bracket · scratched · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > LEFT WING INBD FLAP FORWARD HINGE BRACKET PIVOT BORE OTBD SPOT FACE FOUND SCRATCHED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-07, REVISION 74. REPAIR ACCOMPLISHED PER EA 1-5750-162397, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 1 - [SDR FDEA201211194094](https://openairdocs.org/sdr/FDEA201211194094.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING INBD FLAP, FORWARD HINGE BRACKET PIVOT LUG BORE INBD AND OTBD SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-07 REVISION 74. REPAIR ACCOMPLISHED AS PER EA 1-5750-163542, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6 - [SDR FDEA201211194092](https://openairdocs.org/sdr/FDEA201211194092.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > DURING BUSHING REMOVAL, LEFT WING INBD FLAP, AFT OTBD HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORRODED BEYOND LIMITS. ACCOMPLISHED BUSHING REPAIR PER EA 1-5750-162394 PART 1. REPAIR CLASSIFIED A MAJOR PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211194091](https://openairdocs.org/sdr/FDEA201211194091.md): Skin · chafed · Nov 19, 2012 · N579FE · Doug MD11F · Fuselage Main, Plate/Skin > SKIN CHAFED AT BS 889, LONGERON 40 - 41R. REPAIRED AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 51. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211194090](https://openairdocs.org/sdr/FDEA201211194090.md): Skin · chafed · Nov 19, 2012 · N579FE · Doug MD11F · Fuselage Main, Plate/Skin > SKIN CHAFED BS 1009, LONGERON 40 - 41R. REPAIRED AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 51. EO 1-5100-7-5001 B2 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211194085](https://openairdocs.org/sdr/FDEA201211194085.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND EXCEEDED LIMIT AFTER BUSHING REMOVED. REPAIRED IAW EA 1-5750-75980 REVISION A PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201211194082](https://openairdocs.org/sdr/FDEA201211194082.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING OTBD FLAP INBD FORWARD HINGE BRACKET SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 20-10-6 REVISION 74. FOUND ACCEPTABLE IAW EA 1-5750-162398 PART 1. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 74. REPAIR CARRIED OUT PER E - [SDR FDEA201211194089](https://openairdocs.org/sdr/FDEA201211194089.md): Rib · cracked · Nov 19, 2012 · N579FE · Doug MD11F · Wing, Rib/Bulkhead > ON REMOVAL OF RT WING NR 8 SLAT, CRACKS WERE FOUND ON RIB AT STATION XOS =1141.2. R & R IAW DWG ARB1954 REV NC AND EA 1-5750-163529, STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115. - [SDR FDEA201211194088](https://openairdocs.org/sdr/FDEA201211194088.md): Rib · cracked · Nov 19, 2012 · N579FE · Doug MD11F · Wing, Rib/Bulkhead > ON REMOVAL OF RT WING NR 8 SLAT, CRACKS FOUND ON RIB AT STATION XOS =1146.8. REMOVED AND REPLACED AS PER DRAWING ARB1954 REVISION NC AND E.A. 1-5750-163529 STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211194087](https://openairdocs.org/sdr/FDEA201211194087.md): Rib · cracked · Nov 19, 2012 · N579FE · Doug MD11F · Wing, Rib/Bulkhead > ON REMOVAL OF RT WING NR 8 SLAT, CRACKS FOUND ON RIB AT STATION XOS =1135.6. REMOVED AND REPLACED IAW DRAWING ARB1954 REVISION NC AND EA 1-5750-163529 STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211194086](https://openairdocs.org/sdr/FDEA201211194086.md): Rib · cracked · Nov 19, 2012 · N579FE · Doug MD11F · Wing, Rib/Bulkhead > ON REMOVAL OF RT WING NR 8 SLAT, CRACKS FOUND ON RIB AT STATION XOS =1152.4. REMOVED AND REPLACED IAW DRAWING ARB1955 REVISION D AND EA 1-5750-163529 STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115. - [SDR FDEA201211194083](https://openairdocs.org/sdr/FDEA201211194083.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET LOWER MOUNT OTBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08 REVISION 74. REPAIRED IAW EA 1-5750-162398 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115. - [SDR FDEA201211194081](https://openairdocs.org/sdr/FDEA201211194081.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 6, 9 AND 10. REPAIR CLASSIFIED AS MAJOR - [SDR FDEA201211194080](https://openairdocs.org/sdr/FDEA201211194080.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 6, 9 AND 10,. WASHER AT OUTBOARD HIN - [SDR FDEA201211194079](https://openairdocs.org/sdr/FDEA201211194079.md): Fitting · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE LOAD FITTING LOWER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, AND 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION - [SDR FDEA201211194078](https://openairdocs.org/sdr/FDEA201211194078.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING UPPER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, AND 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV - [SDR FDEA201211194077](https://openairdocs.org/sdr/FDEA201211194077.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING LOWER BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 7, 9 AND 10. REPAIR CLASSIFIED AS M - [SDR FDEA201211194076](https://openairdocs.org/sdr/FDEA201211194076.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING UPPER BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITD AS PER CMM 57-44-09 REVISION 74.. REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 7, 9 AND 10. REPAIR CLASSIFIED AS MA - [SDR FDEA201211194075](https://openairdocs.org/sdr/FDEA201211194075.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET LOWER MOUNT INBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44- 09 REVISION 74.. REPAIRED PER EA 1-5750-162400 PART 1, STEPS 1, 2, 3, 4, 5, 8, 9 AND 10. REPAIR CLASSIFIED AS MAJOR PER - [SDR FDEA201211194093](https://openairdocs.org/sdr/FDEA201211194093.md): Hinge Bracket · corroded · Nov 19, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > RIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE OTBD SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING THICKNESS: 0.263", MATERIAL REMOVED: 0.078", REMAINING THICKNESS: 0.185", MINIMUM THICKNESS: 0. - [SDR FDEA201211174062](https://openairdocs.org/sdr/FDEA201211174062.md): Bracket · corroded · Nov 17, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > LEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. EXISTING HOLE DIAMETER = 1.224 INCH, FINAL HOLE DIAMETER = 1.228 INCH, MAXIMUM HOLE DIAMETER = 1.220 INCH. R - [SDR FDEA201211174065](https://openairdocs.org/sdr/FDEA201211174065.md): Hinge Bracket · corroded · Nov 17, 2012 · N579FE · Doug MD11F · Trailing Edge Flaps > LEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 REVISION 74. REPAIRED PER EA 1-5750-163540 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115. Next page: https://openairdocs.org/deregistered/N579FE-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 = 'N579FE' AND deregistration_id = 'N579FE-2024-03-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N579FE-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.