Mcdonnell Douglas MD-11

Service difficulty reports · 7,956

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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"

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SDR UPS08M51973Skin · chafedINSPECTION TYPE:C RIGHT I/B AILERON FOUND CHAFE MARKS ALONG L/E LOWER SKIN I/B SIDE. CHAFED SKIN REMOVED PER SRM 51-35-01V.2R.40. HOLES ON NEW SKIN PICKED UP PER SRM 51-31-01 V.2 R.40. NEW SKIN INSTALLED AS PER SRM 51-35-01 V.2 R.40.Jan 27, 2008 · N294UP · Doug MD11 · AileronsSDR UPS08M52148Intercostal · crackedINSPECTION TYPE:C CABIN AT STA 1215, ADJACENT LONGERON 27 RT TOP INTERCOSTAL STIFFENER FOUND CRACKED AT FWD EDGE. NEW INTERCOSTAL STIFFENER FABRICATED USING MATL 60-17778X7075T6511 PER EN1069-08. FPI C/OUT IAW BOEING DPS 4.707 REV.AW FOUND NO CRACK EVIDENT. Jan 25, 2008 · N294UP · Doug MD11 · Fuselage Miscellaneous StructureSDR UPS08M52138Seat Track · corrodedINSPECTION TYPE:C CABIN-MAIN DECK SEAT TRACK AT BS 840-BS 859 X=+27.5 (LT) FOUND CORROSION AS MARKED. CORRODED SEAT TRACK FRAME EXISTING SECTION REMOVED PER SRM 51-33-01 V.2R.40. HFEC INSP C/OUT IAW DACNDTSPM R.13 PART06.10.01.001 FOUND NO CRACK EVIDENT. REJan 25, 2008 · N294UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52137Seat Track · corrodedINSPECTION TYPE:C CABIN, MAIN DECK SEAT TRACK AT BS 840-BS859 X=-7.5 (RT) FOUND CORROSION AS MARKED CORRODED SECTION TRIMMED OFF PER SRM 53-70-00 V.1FIG.R.40. HFEC INSP C/OUT IAW DAC NDTSPM 06-10-01.001R.13 FOUND NO CRACK EVIDENT. REPAIR SPLICES AND PLATES FJan 25, 2008 · N294UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52108Fairing · damagedINSPECTION TYPE:C ENG NR 2 EXHAUST FAIRING RT SIDE WITH EXISTING PATCH REPAIR. FPI C/OUT ON EXISTING REPAIR IAW DACNDTSPM R.13 PART08 FOUND NO CRACK EVIDENT ON FAIRING SKIN & REPAIR DOUBLER. NEW REPAIR DOUBLER FAB USING 2219-0 0.071" PER EN 1123-08&MD11-54-2Jan 24, 2008 · N294UP · Doug MD11 · Nacelle/Pylon Miscellaneous StructureSDR WRLA2008014Oven · defectiveOKBK/EDDP. OVEN 509 MID GALLEY INOP BURNING SMELL WHEN USED. REMOVED AND REPLACED MID GALLEY OVEN 509 REF MM 25-33-00. DMI CLOSED.Jan 23, 2008 · N277WA · Doug MD11 · Buffet/GalleysSDR UPS08M52058Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE AFT LOWER O/B BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE LWR MOUNT O/B BORE & SPOTFACE CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08 PG 602-607R.60. FPI C/Jan 21, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52057Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING HINGE MOUNTED SIDE ATTACHMENT UPPER BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE BARREL NUT UPR BORE & SPOTFACE CORROSION REMOVED & FOUND WITHIN LIMIT PER CMM57-44-08 PG 613-615R.6Jan 21, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52056Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE AFT LOWER I/B BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE LWR MOUNT I/B BORE & SPOT FACE CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08 PG602-607R.60. FPI CJan 21, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52054Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE SIDE ATTACHMENT LOWER BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE BARREL NUT LWR BORE & SPOTFACE CORROSION REMOVED & FOUND WITHIN LIMIT PER CMM57-44-08 PG 613-615R.6Jan 21, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52107Stringer · crackedINSPECTION TYPE:C LEFT WING UPPER STRINGER END S9 SUSPECT AS MARKED, THRU ACCESS 38AB. HFEC INSP C/OUT PER DACNDTSPM R.13 PART06.10.01.001&CRACK APPROX 12" FOUND. STR 9 CRACKED AREA TRIMMED OFF PER SRM 57-20-00 FIG 10V.1&EN1055-0 8. NEW STR & 03EA REP PARTSJan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52106Stringer · crackedINSPECTION TYPE:C LEFT WING UPPER STRINGER END S11 SUSPECT CRACK AS MARKED, THRU ACCESS 536AB. HFEC INSP C/OUT PER DACNDTSPM R.13 PART06-10.01.001 & CRACK APPROX 11" FOUND CRACK AT STR 11 LT WING TRIMMED OFF PER SRM 57-20-00 FIG 10V.1&EN1056-08 NEW STR 11 & 0Jan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52105Stringer · crackedINSPECTION TYPE:C RIGHT WING UPPER STRINGER END S-12 SUSPECT CRACK AS MARKED, THRU ACCESS 635BT. HFEC INSP C/OUT PER DAC NDTSPM R.13PART06.10.01.001 & CRACK APPROX 11" FOUND AS MARKED. CRACK AT STR 12 TRIMMED OFF PER SRM 57-20-00 FIG 10V.1 & EN1064-08. NEW Jan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52104Stringer · crackedINSPECTION TYPE:C RT WING UPPER STRINGER END NR S9 SUSPECT CRACK AS MARKED, THRU ACCESS NR 638AB. HFEC INSP CARRIED OUT PER DACNDT SPM R.13 PART06.10.01.001 AND CRACK APPROX 9 INCH FOUND AS MARKED. CRACK AT RHW STR NR 9 SLOTTED OUT PER SRM 57-20-00 FIG 10V.1Jan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52103Stringer · crackedINSPECTION TYPE:C RT WING UPPER STRINGER END NR S10 SUSPECT CRACK AS MARKED, THRU ACCESS NR 636CB. HFEC INSP CARRIED OUT PER DAC NDT SPM R.13 PART06.10.01.001 AND CRACK APPROX 11 INCHES FOUND AS MARKED. CRACK AT RHW STR NR 10 SLOTTED OUT PER SRM 57-20-00 FIGJan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52102Stringer · crackedINSPECTION TYPE:C LT WING UPPER STRINGER END NR S12 SUSPECT CRACK AS MARKED THRU ACCESS NR 535BT. HFEC INSP CARRIED OUT PER DAC NDT SPM R.13 PART 06.10.01.00 AND CRACK APPROX 7 INCHES FOUND. CRACK AT LHW STR NR 12 SLOTTED OUT PER SRM 57-20-00 FIG 10 V.1R.35.Jan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52101Stringer · crackedINSPECTION TYPE:C RT WING UPPER STRINGER END S11 SUSPECT CRACK AS MARKED THRU ACCESS NR 636AB. HFEC INSP C/OUT PER DAC NDTSPM R.13 PART06.10.01.001 AT UPPER STRINGER END NR S11 AND CRACK APPROX 9 INCH FOUND. CRACK AT RHW STR NR 11 SLOTTED PER SRM 57- 200-00 Jan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52151Structure · bentINSPECTION TYPE:C EVALUATE CENTER CARGO DOOR C2 LOWER EDGE BENT BACK TO ORIGINAL CONTOUR PER DELTA ERA 36046-1-14. CORNER DOUBLER FAB FR MATL 7075-0-0.063" PER DWG ADA3774 AND REPAIR ANGLE FAB FR MATL 7075-0-0.080" PER EN1085-08. CORNER DOUBLER AND REPAIR ANJan 17, 2008 · N294UP · Doug MD11 · Cargo/Baggage DoorsSDR UPS08M51580Seat Track · corrodedINSPECTION TYPE:C CABIN-SEAT TRACK CROWN AREA AT STA 1341-1361, X=-107 FOUND CORROSION AS MARKED. CORROSION AT CABIN STA 1341-1361 X=-107 ON SEAT TRACK CROWN AND UPPER LEG AREA REMOVED PER SRM 51-21-01 V.II R35, FOUND EXCEEDED LIMITS PER SRM 5 3-70-00 FIG 3 VJan 17, 2008 · N293UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52011Structure · damagedINSPECTION TYPE:C LT WING OUTBOARD FIXED L/E AT NR 8 SLAT 13 INCHES LONG GROOVE WORN FROM CONTACT WITH SEAL RETAINER, OUT OF LIMITS. GROOVE MARK REWORKED PER SRM 51-21-01V.2R35 ORIG THK:0.040", MAT`L REMVD :0.007", MATL REM:0.033" FOUND EXCEED LIMIT PER SRM 5Jan 15, 2008 · N294UP · Doug MD11 · Wing Main, Frame StructureSDR CO1Y200800003Hinge Bracket · wornLT SPOILER NR1 FOUND WITH PLAY.Jan 14, 2008 · N725BC · Doug MD11 · SpoilersSDR UPS08M51548Skin · crackedFUSELAGE SKIN REPAIR AT BS 1925 BETWEEN L45R AND L48L. INSTALLED TRIPLER REPAIR PER EO MD11-5330-28480 AND EA011-5330- 01-A1261.Jan 14, 2008 · N258UP · Doug MD11 · Fuselage Main, Plate/SkinSDR UPS08M51720Doubler · crackedINSPECTION TYPE:C LEFT WING FIXED L/E COMPT AT STA XORS 558 APPROX FOUND UPPER DOUBLER CRACK AS MARKED. I/B & O/B RIB AT LEFT WING FIXED L/E COMPT AT XORS 558 AREA REMOVED FOR ACCESS AS PER SRM 51-31-01 V.II R35. FASTENERS AT CRACKED AREA AT LEFT WING L/E FIJan 10, 2008 · N293UP · Doug MD11 · Wing Miscellaneous StructureSDR UPS08M51681Doubler · crackedINSPECTION TYPE:C LEFT WING FIXED L/E COMPT AT STA XORS 500 APPROX FOUND UPPER DOUBLER SUSPECTED CRACK AS MARKED. HFEC INSP C/O PER NDTSPM 06-10-01.001 R13 ON SUSPECTED CRACK AREAS & FOUND APPROX 1/4 CRACK AS MARKED. INBOARD & OUTBOARD RIB AT LEFT FIXED L/E Jan 10, 2008 · N293UP · Doug MD11 · Wing Miscellaneous StructureSDR WRLA2008012Angle · corrodedDURING C-CHECK INSPECTION FOUND CORROSION ON LOWER CHORD AT STA Y=1964 L48L. BLENDED CORROSION, AREA MEASURED WITHIN LIMITS PER SRM VOL.1 53-00-01 FIG.3 REV.40.Jan 10, 2008 · N277WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2008009Seat Track · corrodedDURING C-CHECK INSPECTION FOUND SEAT TRACK CORROSION AT STA Y=840 TO 859 X=14. BLENDED CORROSION, WITHIN ALLOWABLE LIMITS PER MD11 SRM VOL.1 53-00-01 FIG.3 REV.40. REF EGAT NRCU 05022.Jan 10, 2008 · N277WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2008008Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= 56.65. REPLACED AFT FLOOR SUPPORT PER MD11 SRM VOL.II 51-35-01 FIG.1 REV.40.Jan 7, 2008 · N277WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2008007Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2000, X= -56.65. REPLACED AFT FUSELAGE FLOOR SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40.Jan 6, 2008 · N277WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2008006Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= -27.5. REPLACED AFT FUSELAGE FLOOR SUPPORT PER MD-11 VOL.II 51-35-01 FIG.1 REV.40.Jan 5, 2008 · N277WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2008005Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X=27.5. REPLACED AFT FLOOP SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40.Jan 5, 2008 · N277WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2008004Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= 23.5. REPLACED AFT FLOOR SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40.Jan 5, 2008 · N277WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2008003Floor Support · corrodedDURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= -23.5. REPLACED AFT FUSELAGE FLOOR SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40.Jan 5, 2008 · N277WA · Doug MD11 · Fuselage Miscellaneous StructureSDR UPS08M51826Skin · corrodedINSPECTION TYPE:C LT WING I/B FLAP LOWER SURFACE I/B AND O/B SEGMENT FOUND SURFACE CORROSION AS MARKED. LHW I/B FLAP I/B AND O/B SEGMENT LOWER SURFACE SKIN REMOVED PER SRM 51-3 1-01 V.II R35. NEW LHW INBOARD FLAP I/B AND O/B SEGMENT LOWER SURFACE SKIN FAB PEJan 4, 2008 · N293UP · Doug MD11 · Trailing Edge FlapsSDR 08FDEA00031Skin · dentedRIGHT WING - INBOARD FLAP UPPER SURFACE FOUND DENT AT XIFH 193. REPAIR CARRIED OUT AT RIGHT HAND WING INBOARD FLAP UPPER SURFACE AT XIFH 193 AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jan 4, 2008 · N592FE · Doug MD11 · Trailing Edge FlapsSDR WRLA2008002Access Panel · crackedDURING C-CHECK INSPECTION FOUND RT WING OUTBOARD SLAT DRIVE MECHANISM ACCESS PANEL SKIN CRACKED. REPAIRED RT WING ACTUATOR ACCESS DOOR OUTER SKIN AT XOS STA 490.85 PER EGAT EI NR W2008A57B-022.Jan 4, 2008 · N277WA · Doug MD11 · Wing, Plate/SkinSDR UPS08M51827Skin · crackedINSPECTION TYPE:C LHW LE FIXED WING APPROX STA XORS 577 INNER SKIN FOUND CRACKED. FASTENERS AT CRACKED AREA AT LHW LE FIXED WING STA XORS 577 INNER SKIN AREA REMOVED PER SRM51-35-01 V.II R35 AND CRACKED AREA AT XORS 577 TRIMMED OUT PER SRM 57-10-00 V.I FIG R4Jan 3, 2008 · N293UP · Doug MD11 · Leading Edge DevicesSDR WRLA2008001Skin · crackedDURING C-CHECK INSPECTION FOUND CRACK ON RIGHT FWD AIR CONDITION COMPARTMENT DOOR OUTER SKIN UPPER EDGE APPROX 4.5 INCHES. REPAIRED PER MD-11 SRM 52-10-00 VOL.I REV.40.Jan 2, 2008 · N277WA · Doug MD11 · Air Conditioning DoorsSDR UPS08M51680Stiffener · crackedINSPECTION TYPE:C RIGHT WING FIXED L/E COMPT AT STA XORS 690 APPROX FOUND STIFFENER CRACK AS MARKED. CRACKED STIFFENER AT RT WING FIXED L/E COMPT AT STA XORS 690 AREA REMOVED PER SRM 51-31-01 V.II R35. NEW STIFFENER FAB PER DWG ARB2923-4. HOLES TRANSFERRED Dec 30, 2007 · N293UP · Doug MD11 · Fuselage Miscellaneous StructureSDR UPS08M51436Seat Track · corrodedINSPECTION TYPE:C MAIN DECK AFT ZONE, LBL 27.5 SEAT TRACK BADLY CORRODED BETWEEN STA 1671 & STA 1771. CORROSION AT MAIN DECK BETWEEN STA 1671 TO 1771 LBL 27.5 ON SEAT TRACK CROWN BASE & FLANGE AREA. REMOVED PER SRM 51-21-01 VII R35 FOUND EXCEEDS LIMITS PER SDec 27, 2007 · N293UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M51511Intercostal · crackedINSPECTION TYPE:C CABIN, LONGERON L7 RT AT STA 515-535, FOUND INTERCOSTAL CRACK AS MARKED. CRACK INTERCOSTAL AT CABIN LONGERON L7 RT AT STA 515-535 AREA. REMOVED PER SRM51-31-V.II R35. NEW INTERCOSTAL P/N:AFA3087-17 FAB PER DWG AF A3087. HOLES ON FAB INTERDec 25, 2007 · N293UP · Doug MD11 · Fuselage Miscellaneous StructureSDR UPS08M51707Panel · damagedINSPECTION TYPE:C EMPENNAGE, LT HORIZONTAL STABILIZER FRONT SPAR, TOP OF ACCESS PANEL 331B Z CUTOUT AREA, UPPER SURFACE MOUNTING HOLES FOR L/E PANEL 331BT, FOUND WITH 01 EA ELONGATED MOUNTING HOLE AS MARKED. GANG CHANNEL ASSY PARTIALLY REMOVED FOR ACCESS PER Dec 21, 2007 · N293UP · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR UPS08M51706Panel · damagedINSPECTION TYPE:C EMPENNAGE, LT HORIZONTAL STABILIZER FRONT SPAR, TOP OF ACCESS PANEL 331A Z CUTOUT AREA, UPPER SURFACE MOUNTING HOLES FOR L/E PANEL 331BT, FOUND WITH 11 EA ELONGATED MOUNTING HOLES AS MARKED. GANG CHANNEL ASSY REMOVED FOR ACCESS PER SRM 51-35Dec 21, 2007 · N293UP · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR UPS08M51608Stringer · crackedINSPECTION TYPE:C LT WING TANK UPPER STRINGER NR 10 SUSPECT CRACK AS MARKED, THRU TANK LOWER ACCESS NR 536CB. HFEC INSP C/O PER DAC NDTSPM REV 13 PT 6 06-10-01.01.001 AND FOUND CRACK APPROX 10 INCHES AS MARKED. LT WING TANK UPPER STRINGER NR 10 ATTACHED SPLIDec 18, 2007 · N293UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M51531Stringer · crackedINSPECTION TYPE:C RT WING UPPER STRINGER END NR 12 SUSPECT CRACK AS MARKED, THRU TANK ACCESS NR 635BT, RHW UPPER STRINGER NR 12 ATTACHED SPLICE REMOVED FOR ACCESS. HFEC INSP C/O PER DAC NDT SPM R13, 06-10-01.001 AND FOUND CRACK END APPROX 8". CRACK AREA SLOTDec 18, 2007 · N293UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M51595Skin · damagedINSPECTION TYPE:C CENTER CARGO DOOR CUTOUT AFT LWR CORNER FOUND PREVIOUS REPAIR AND WITH RUSTY FASTENERS. PREVIOUS REPAIR DOUBLER REMOVED PER SRM 51-31-01 V.II R35. HFEC INSP C/O PER DAC NDTSPM REV 13 06-10-01.001 ON EXISTING TRIMMED OFF AREA (02EA) AND FOUNDec 17, 2007 · N293UP · Doug MD11 · Fuselage Main, Plate/SkinSDR UPS08M51554Skin · dentedINSPECTION TYPE:C CENTER CARGO DOOR CUTOUT AFT AREA STA 1790.0 RT L36 FOUND DENT AS MARKED DENT AREA SMOOTHED OUT PER SRM 51-21-01 V.II R35. DENT MARK MEASURED FOUND BEYOND LIMIT PER SRM 53-20-00 FIG 6 V.I R35. HFEC INSP CARRIED OUT PER DAC NDTSPM R.13 06-10Dec 17, 2007 · N293UP · Doug MD11 · Fuselage Main, Plate/SkinSDR UPS08M51508Floor Support · corrodedINSPECTION TYPE:C AFT CARGO/AT STATION 1841 TO STATION 1900 RT MOST OUTBOARD FLOOR SUPPORT FOUND WITH SURFACE CORROSION. CORROSION SUPPORT REMOVED PER SRM51-31-01 V.II R35. NEW SUPPORT P/N:AGA 3857-412 FAB PER DWG AGA3857. SUPPORT HEAT TREAT TO T62 COND PERDec 16, 2007 · N293UP · Doug MD11 · Fuselage Miscellaneous StructureSDR UPS08M51438Seat Track · corrodedINSPECTION TYPE:C MAIN DECK FLOOR, RBL 75 SEAT TRACK CROWN & FLANGE FOUND CORRODED BETWEEN STA 1341 & STA 1381. CORROSION AT MAIN DECK BETWEEN STA 1341 TO STA 1381 RBL ON SEAT TRACK CROWN BASE & FLANGE AREA REMOVED PER SRM 51-21-01 VII R35 & FOUND EXCEED LIMIDec 16, 2007 · N293UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M51510Intercostal · crackedINSPECTION TYPE:C CABIN, INTERCOSTAL AT STA 1621-1641,L7 RT FOUND CRACKED AS MARKED. CRACKED INTERCOSTAL AT CABIN STA 1621 TO 1641 LONGERON L7 AREA. REMOVED PER SRM 51-31-01 V.II R35. NEW INTERCOSTAL FAB PER BOEING DWG AFA7761. FAB INTERCOSTAL FASTENERS HODec 14, 2007 · N293UP · Doug MD11 · Fuselage Miscellaneous StructureSDR UPS08M51509Intercostal · crackedINSPECTION TYPE:C CABIN, INTERCOSTAL AT STA 1701-1721, L7 RT FOUND CRACKED AS MARKED. CRACKED INTERCOSTAL AT CABIN STA 1701-1721 LONGERON L7 AREA REMOVED PER SRM51-31-01 V.II R35. NEW INTERCOSTAL P/N:AFA7761-25 FAB PER BOEING DWG AFA7761. FAB INTERCOSTAL FADec 14, 2007 · N293UP · Doug MD11 · Fuselage Miscellaneous Structure
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