Mcdonnell Douglas MD-11

Service difficulty reports · 7,956

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'MD11'
  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 07FDEA02013Skin · corrodedMAIN DECK L3 DOOR CUTOUT FORWARD LOWER CORNER FOUND CORRODED. MAIN DECK L3 DOOR CUTOUT FORWARD LOWER CORNER CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 29, 2007 · N576FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 07FDEA02012Skin · corrodedAPU - FUSELAGE SKIN EXTERIOR AT APU EXHAUST DOOR LOWER SIDE HINGE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5330-109892. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 29, 2007 · N576FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 07FDEA02011Skin · dentedFORWARD CARGO AFT LOWER CUTOUT SKIN FOUND DENT. [06-12-07] DENT AT FORWARD CARGO AFT LOWER DOOR CUTOUT SKIN TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 29, 2007 · N576FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 07FDEA01992Stringer · crackedCTR CARGO: UNDER FLOOR STA 1821, RT X=56 FOUND STRINGER JOINT END CRACKED. [06-19-07] REPAIR CARRIED OUT AT CTR CARGO: UNDER FLOOR STA 1821, STRINGER S43R JOINT END AS PER SRM 51-33-01 VOLUME II.May 29, 2007 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS07M50115Structure · corrodedINSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT NR 25 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIUSED SMMay 28, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50114Structure · corrodedINSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 22 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIUSMay 28, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50284Skin · crackedINSPECTION TYPE:C LT FIXED LE LWR COMPT UPPER SKIN DOUBLER SUSPECTED CRACK AT STA XORS 535. HFEC INSP CARRIED OUT PER DAC NDTSPM R.13 PART 06-10-01-001 FOUND CRACK AS MARKED. REPAIR ANGLES FAB AND CRACK AREA TRIM OFF PER EN1375-07. REPAIR ANGLES HEAT TREATEMay 25, 2007 · N260UP · Doug MD11 · Wing, Plate/SkinSDR 07FDEA02005Control Unit · failedAT APPROX 00:00Z GOT A MASTER WARNING LT W/A LEVEL 1 EMERGENCY POWER ON ALERT. COMPLIED W/QRH. SELECTED EMERGENCY POWER SWITCH TO OFF. GOT LVL 1 L EMERGENCY AC BUSS ALERT. SELECTED EMERGENCY POWER SWITCH BACK TO ARM , STILL HAD EMERGENCY POWER ON LEVEL ONMay 25, 2007 · N605FE · Doug MD11 · AC Generation SystemSDR WRLA2007069Fan · failedFLIGHT 8011 KBAD/PHIK 05/25/07 - DURING CRUISE FLT350 ELECTRICAL FUMES REPORTED BY CABIN CREW IN A ZONE. COMPLIED WITH VOL 1 PROCEDURES. FUMES DISSIPATED WHEN CAB BUSS SWITCH SELECTED OFF. PAX REPORTED HIGH PITCHED NOISE FROM LEFT REAR WALL OF -A ZONE- UNKNMay 25, 2007 · N801DE · Doug MD11 · Air Distribution FanSDR UPS07M50108Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 16 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSEMay 22, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50107Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 7 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSEDMay 22, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50302Longeron · corrodedINSPECTION TYPE:C CTR CARGO THRU STATION 1661, LONGERON R48 FOUND WITH CORROSION AS MARKED. CORROSION REMOVED FOUND EXCEEDS PER SRM 53-00-01V.1R.38. REPAIR ANGLES FAB AND FASTENER HOLES PICK UP PER EN1355-07. REP ANGLES 02EA AND REWORK AREA REPROTECTED AND May 21, 2007 · N260UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS07M50113Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 22 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSEMay 21, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50106Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 19 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSEMay 21, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR 07FDEA01919Frame · damagedMAIN DECK CARGO COMPARTMENT, LEFT MAIN FRAME STA 1661 EXISTING REPAIR DOUBLER AT LONGERON 12L FOUND DAMAGED. MAIN DECK CARGO COMPARTMENT, LEFT FUSELAGE MAIN FRAME STA 1661 DAMAGED EXISTING REPAIR DOUBLER AT LONGERON 12L REMOVED AND REPLACED. REPAIR CARRIEDMay 21, 2007 · N613FE · Doug MD11 · Fuselage Main, FrameSDR UPS07M50094Seat Track · corrodedINSPECTION TYPE:C CABIN-SEAT TRACK BETWEEN STA889-919 RBL=107 FOUND CORRODED. REMOVAL C/OUT ON SEAT TRACK AREA TO EXECUTE REPAIR AS NECESSARY. REPAIRED S/TRACK SPLICE HAT AND SPLICE PLATE FAB PER SRM 53-70-00.V2.R 38. PICKED UP HOLES FOR FAB PARTS PER SRM 5May 18, 2007 · N260UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M50112Structure · corrodedINSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 23 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSEMay 15, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR WRLA2007068Panel · damagedFLT 8129/LEJ/ATL 05/15/2007. ON POST FLIGHT INSPECTION WORLD AIRWAYS MAINTENANCE FOUND LEFT WING REFUEL PANEL DAMAGED AND PINCHED BY NR 4 LEADING EDGE SLAT. REMOVED LEFT WING FUELING PANEL DOOR, TRIMMED OUT DAMAGE, INSPECTED PER DELTA AIR LINES ERA 461879-14May 15, 2007 · N273WA · Doug MD11 · Wing, Plate/SkinSDR 07FDEA01783Wedge · delaminatedRIGHT WING OUTBOARD FLAP INBOARD WEDGE TRAILING EDGE UPPER SURFACE FOUND DELAMINATED RIGHT WING OUTBOARD FLAP INBOARD WEDGE REMOVED AND REPLACED AS PER AMM 20-50-02, P/N ON: ARC4363-2, S/N ON: 177679-9.May 14, 2007 · N574FE · Doug MD11 · Trailing Edge FlapsSDR UPS07M50105Structure · corrodedINSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 36 FOUND CORRODED. ACCESS CUT AT UPPER TORQUE BOX WEB. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEED LIMITS. DVI C/OUT FOUND NO CORROSION. REPAIR SLEEVE BUSHING, DOUBLERMay 11, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50111Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT NR 23 FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSED SMOMay 10, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50110Structure · corrodedINSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT NR 30 FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIUSED SMMay 10, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50104Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT NR 20 FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSED SMOMay 10, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50073Web · crackedINSPECTION TYPE:C COCKPIT, 1ST OBSERVER SEAT SUPPORT WEB FOUND CRACKED. COCKPIT 1ST OBS SEAT SUPPORT WEB CRACKED AREA TRIMMED OFF PER SRM 53-00-01 VOLI REV 39. HFEC INSP C/OUT ON TRIMMED OFF AREA, NO CRACK REINFORCED DOUBLER FAB PER SRM 53-00-01 VOLI FIG 6 RMay 8, 2007 · N288UP · Doug MD11 · Fuselage Main, StructureSDR UPS07M50101Structure · corrodedINSPECTION TYPE:C EMPENNAGE/LT HORIZONTAL STABILIZER BARREL NUT NR 24 LT FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, BOTTOM REMAINING BLEND OUT EXCEEDS LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERYMay 7, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50100Structure · corrodedINSPECTION TYPE:C EMPENNAGE/LT HORIZONTAL STABILIZER BARREL NUT NR 15 LT FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, BOTTOM REMAINING BLENDED OUT EXCEEDS LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUTS AND BOTTOM PERIPHERY RAMay 7, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50099Structure · corrodedINSPECTION TYPE:C EMPENNAGE/LT HORIZONTAL STABILIZER BARREL NUT NR 9 LT FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, BOTTOM REMAINING BLENDED OUT EXCEEDS LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERYMay 7, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50109Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT NR 2 RT FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT AND BOTTOM PERIPHERY RADIUSED SMOOTHMay 6, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50098Structure · corrodedINSPECTION TYPE:C EMPENNAGE/RT HORIZONTAL STABILIZER BARREL NUT NR 15 RT FOUND BORE C CORRODED. CORROSION AT BARREL NUT BORE REMOVED, BOTTOM SURFACE REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT, BOTTOM May 6, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR WRLA2007066Drive Assy · shearedAIR RETURN. AFTER TAKEOFF CAPTAIN AND FIRST OFFICER FOUND LONGITUDINAL TRIM HANDLE WOULD NOT TRIM THE HORIZONTAL STAB. STAB REMAINED AT 7.6 UNITS OF TRIM. AUTOPILOT LEFT AND RIGHT DID NOT AFFECT TRIM POSITION. DURING PRESENT AND MODERATE PITCH CHANGE FELT May 6, 2007 · N271WA · Doug MD11 · Stabilizer Position IndicatingSDR 07FDEA01710Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1042. [SUP 05-22-07] REPAIRED AS PER FEDEX EA 1-5710-111099.May 6, 2007 · N606FE · Doug MD11 · Wing SparSDR UPS07M50071Doubler · crackedINSPECTION TYPE:C RT WING, FIXED L/E INTERIOR FOUND BEADED DOUBLER CRACKED BETWEEN XOS 698 TO XOS 703 AS MARKED. RIBS AT RHW FIXED L/E REPAIR AREA REMOVED. CRACK AREA TRIMMED OFF PER SRM 57-10-00 FIG 27 VOLI REV 39. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUNDMay 5, 2007 · N288UP · Doug MD11 · Leading Edge DevicesSDR 07FDEA01692Skin · crackedRIGHT WING, LEADING EDGE LOWER SURFACE 619CB PANEL FWD I/B SIDE CORNER FOUND 5/8 INCH CRACK AT XOS 607. [SUP 05-22-07] REPAIR CARRIED OUT AT RIGHT WING - LEADING EDGE LOWER SURFACE 619CB PANEL FWD I/B SIDE CORNER, XOS 607 AS PER SRM 57-10-00 FIGURE 21 VOMay 3, 2007 · N606FE · Doug MD11 · Wing, Plate/SkinSDR 07FDEA01691Hinge Fitting · crackedTAIL CONE COMPARTMENT, LT HINGE FITTING FOUND CRACKED, VIEWED FROM AFT ACCESSORY COMPARTMENT. [SUP 05-14-07] REMOVED & REPLACED AS PER DAC DWG AJC7346 AND SRM 51-31-01 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.May 3, 2007 · N574FE · Doug MD11 · Aerodynamic FairingsSDR 07FDEA01690Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.656". [SUP 05-14-07] COMPLIED WITH FEDEX EA 1-5750-109875, May 3, 2007 · N574FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01689Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.657". [SUP 05-14-07] COMPLIED WITH FEDEX EA 1-5750-109875,May 3, 2007 · N574FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01688Skin · delaminatedRIGHT WING OUTBOARD FLAP CENTER TRAILING EDGE LOWER SURFACE FOUND DELAMINATED 4" BY 4" (LENGTH X WIDTH). [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 20-50-02.May 3, 2007 · N574FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01687Skin · delaminatedRIGHT WING, OUTBOARD FLAP INBOARD TRAILING EDGE UPPER SURFACE FOUND DELAMINATED 5" BY 7" (LENGTH X WIDTH). REMOVED AND REPLACED AS PER AMM 20-50-02. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.May 3, 2007 · N574FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01686Frame · chafedFOUND LEFT MAIN FRAME STA 535 AT 9G NET SUPPORT YOKE AREA FOUND CHAFFED AT LONGERON 23L. [SUP 05-10-07] REPAIR CARRIED OUT AS PER FEDEX AIRCRAFT ENGINEERING STANDARD REWORK DRAWING NR: SRZ 53-503. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 3, 2007 · N574FE · Doug MD11 · Fuselage Main, FrameSDR 07FDEA01665Hinge Fitting · corrodedLT WING OUTBD FLAP INBD HINGE SUPPORT FITTING OUTBD AND 1 BOLT HOLE FOUND CORROSION. LT WING OUTBD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094 - WINGS, LT WING Apr 30, 2007 · N623FE · Doug MD11 · Leading Edge DevicesSDR 07FDEA01667Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE AFT SUPPORT FITTING AFT BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.Apr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01666Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE AFT SUPPORT FITTING FORWARD BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.Apr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01664Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING INBOARD NR 1 BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.Apr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01663Strut · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING AFT STRUT (P/N: ARC2126) FWD AND AFT HOLE FOUND CORRODED. [SUP 05-15-07] COMPLIED WITH FEDEX E.A. 1-5750-111092.Apr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01662Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORRODED. [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5. COMPLY WITH FEDEX EA 1-5710-111094. REPAIR CApr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01661Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING INBOARD NR 2 BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.Apr 30, 2007 · N623FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA01659Angle · crackedRIGHT WING, LEADING EDGE CAVITY AT ABOUT XOS 659 STRIP ANGLE FOUND WITH APPROX 0.5 INCH CRACKED. [SUP 05-14-2007] FIXED LEADING EDGE STRINGER, CRACK REPAIR. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Apr 28, 2007 · N574FE · Doug MD11 · Wing Miscellaneous StructureSDR 07FDEA01658Angle · crackedRIGHT WING, LEADING EDGE CAVITY AT ABOUT XOS 774 STRIP ANGLE FOUND WITH APPROX 0.3124 INCH CRACKED. [SUP 05-14-07] RT FIXED LEADING EDGE STRINGER, CRACK REPAIR. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100.Apr 28, 2007 · N574FE · Doug MD11 · Wing Miscellaneous StructureSDR 07FDEA01657Link · wornCENTER LANDING GEAR, WHEEL WELL BRACKET LOCK LINK CHAMPER FOUND WORN. [SUP 05-04-07] REPAIRED AS PER SRM 53-40-00 VOLUME I, FIGURE 10. REPAIR CALSSIFIED AS MINOR PER GMM 6-2-100.Apr 28, 2007 · N574FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 07FDEA01643Skin · gougedRIGHT WING, LEADING EDGE SLAT NR 3 TRAILING EDGE LOWER SURFACE FOUND WITH GOUGE MARK. [SUP 05-16-07] SURFACE SMOOTHENED OFF AND REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Apr 26, 2007 · N574FE · Doug MD11 · Leading Edge Devices
Back to Mcdonnell Douglas MD-11