N294UP

Service difficulty reports · 369

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

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 n_number = 'N294UP' AND registry_match = 'registration'
  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 IPXA11M67480Accumulator · lowFOUND R1 DOOR EMERGENCY ACCUMULATOR PRESSURE TO ZERO. PRESSURIZED R1 DOOR PNEUMATIC STORAGE AS REQUIRED IAW MM 12-25-04-3.Jun 22, 2011 · N294UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA11M67276Skin · damagedLIGHTNING STRIKE UPPER RUDDER RT SIDE APPROX 10" FROM TOP. REPAIRED IAW EO MD11-5540-43137-A.Jun 16, 2011 · N294UP · Doug MD11F · Rudder, Plate/SkinSDR IPXA1M66730Intercostal · crackedFWD FUSELAGE INTERCOSTAL CRACKED AT STA 555, STR 35R. REPAIRED IAW EO MD11-5310-42749-A.May 19, 2011 · N294UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA11M63961Skin · damagedRT INBD FLAP LOWER SKIN DAMAGED. REPAIRED IAW EO MD11-5750-40699-D.Jan 2, 2011 · N294UP · Doug MD11F · Trailing Edge FlapsSDR IPXA10M62471Power Supply · inoperativeFAILED EMERGENCY LIGHT TEST ON PREFLIGHT. REPLACED POWER SUPPLY IAW MM 33-51-01-4. OPS CHECKS GOOD.Sep 3, 2010 · N294UP · Doug MD11F · Emergency LightingSDR IPXA10M62330Light · failedPDC FOUND EMERGENCY LIGHTS SYS FAIL. REPLACED POWER SUPPLY UNIT AND CHECKED, NO HELP. ITEM DEFERRED IAW MEL 33-50-04. D ITEM M 433618. PLACARD INSTALLED. PERFORMED FUNCTION TEST OF THIS EMERGENCY LIGHTING SYS IAW MM 33-50-00-5. OPS CHECKS NORMAL.Sep 1, 2010 · N294UP · Doug MD11F · Emergency LightingSDR IPXA0M61915Bracket · failedON APPROACH, NR 3 SLAT PULLEY DRUM BRACKET FAILED CAUSING DMG TO NR 3,4 & 5 SLATS. DMG TO NR 3 SLAT CABLES. DMG TO 437 AND 443 L/E RIBS. REPAIRED RIBS IAW MD11-5710-39106-A AT XOS-443, MD11-5710-39117-A AT X OS437. R & R NR 3 SLAT AND NR4 SLAT, REPAIRED NRAug 8, 2010 · N294UP · Doug MD11F · Leading Edge DevicesSDR IPXA10M60663Skin · delaminatedINSPECTION TYPE:2C, IAW CUSTOMER REQUEST REPAIR LT INBD DETACHABLE ELEV. OPENED LT INBD DETACHABLE ELEV AFT INBD CORNER OF SKIN AND REPAIRED 2 EA STIFFENERS REF SRM 55-20-80 REPAIR 1, PARA 4. CLOSED SKIN REF DWG ALC 8940. PRIMED AND TOP COAT IAW SRM 51-21-Jun 14, 2010 · N294UP · Doug MD11F · Elevator, Plate/SkinSDR IPXA0M60618Longeron Fitting · crackedINSPECTION TYPE:2C, LONGERON 46L SPLICE FITTING CRACKED BETWEEN STA 1522-1542. REMOVED, FABRICATED AND INSTALLED LONGERON SPLICE FITTING.Jun 5, 2010 · N294UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA0M60619Longeron Splice · corrodedINSPECTION TYPE:2C, LOWER FWD CARGO LONGITUDINAL SKIN SPLICE LONGERON 48LT HAS EXFOLIATION CORROSION AT STA 1129/6-47. REMOVED CORROSION, CUTOUT LONGERON, FABRICATED AND INSTALLED LONGERON REPLACEMENT SECTION IAW SRM 53-00-05-05, REPAIR 1, FIG. 202.Jun 4, 2010 · N294UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA10M60656Floorbeam · corrodedINSPECTION TYPE:2C, AFT WASTE COMPARTMENT HAS CORROSION ON FLOORBEAM AND CUSP WEB AT INTERSECTION OF FLOORBEAM AT STA 1964 AND CUSP WEB LBL 75. REMOVED CORROSION IN LIMITS ON FLOORBEAM, REMOVED AND FABRICATED, AND INSTALLED WEB CUSP IAW SRM 51-31-01, 51-35-01Jun 3, 2010 · N294UP · Doug MD11F · Fuselage Main, Floor BeamSDR IPXA10M60655Skin · damagedINSPECTION TYPE:2C, DEFERRED ITEM D-416631- CTR LOWER CUT OUT CARGO DOOR BLEND OUT INTERIM REPAIR. REMOVED REPAIR, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLERS IAW STASA EA 011-5330-01-A2481 I/R AND EO MD11-5330-36181-E.Jun 1, 2010 · N294UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA10M60481Skin · dentedINSPECTION TYPE:1C, CONVES DENT LOCATED ON LT FUSELAGE EXTERIOR, APPROX FUSELAGE STA 2204. REMOVED DAMAGE, FABRICATED AND INTALLED REPAIR DOUBLER IAW SRM 53-00-01, FIG. 201.Jun 1, 2010 · N294UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA09M56950Skin · damagedINSPECTION TYPE:N/A SMALL BENT AREA AT THE TOP AFT EXTERIOR SURFACE OF THE L1 DOOR. REPAIRED EXTERIOR SURFACE OF THE L1 DOOR PER EO MD11-5210-34409-B / SRM 52-10-01 REPAIR 3.Aug 9, 2009 · N294UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA09M56955Skin · damagedMX DISCOVERED A SMALL BENT AREA AT THE TOP AFT EXTERIOR SURFACE OF THE L1 DOOR. TRANSFERRED TO NR 345870. COMPLETED PERMANENT REPAIR ON NRC 345870 REF ITEM 2 255716. THIS CLEARS D405541.Jul 28, 2009 · N294UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA09M57087Doubler · gougedINSPECTION TYPE:1C REPAIR SEQ 296-F1-05 EXTERNAL DOUBLER IS GOUGED BETWEEN STA 999 AND STA 1019, L38R-L43R. REMOVED EXISTING REPAIR AT STA 1002.3 FROM L38R-L43R. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF REV 41 MD11 SRM 53-00-15 REPAIR 8.Jul 26, 2009 · N294UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA09M56444Skin · damagedINSPECTION TYPE:SV LT WING LWR SKIN APPROX XOS 650 HAS ELONGATED FASTENER HOLE APPROX 2 INCHES AFT OF L/E OF WING REF NRC 344110. FABRICATED AND INSTALLED REPAIR IAW SAA EA 011-5730-01-A1846 AND IPXA EO MD11-5730-33931-A REF NRC 344110.Jun 18, 2009 · N294UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M56443Skin · damagedINSPECTION TYPE:SV LT WING L/E XOS 621-629 CENTER REPAIR CUTOUT HAS OBLONG FASTENER HOLE AT LWR I/B CORNER OF RIVET PATTERN REF NRC 344110. FABRICATED AND INSTALLED REPAIR IAW SAA EA 011-5730-01-A1846 AND IPXA EO MD11-5730-33931-A REF NRC 344110.Jun 17, 2009 · N294UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M56384Skin · misrepairedINSPECTION TYPE:SV REMOVE EXISTING REPAIRS FROM LT WING AT XOS 609-621, XOS 621-629, AND XO XOS 629-644. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLERS PER EA 011-5730-01-A 1846.Jun 16, 2009 · N294UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M54960Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ. 294-F2-01 ON CENTER MLG IS SUPPECTED PPD LOCATED AT STA 1441 RBL 23.250. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS E.O. MD11-5330-32609-AMar 2, 2009 · N294UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA09M54966Slat · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ 294-W4-001, EXISTING REPAIR DOUBLER ON RT WING NR 8 SLAT EXTENDS BEYOND AUX SPAR WEB TO THE EDGE OF OUTER SKIN LWR SIDE AND NOT PER SRM AND NOT ON MRCSSR REPORT. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER, FIFeb 24, 2009 · N294UP · Doug MD11F · Leading Edge DevicesSDR IPXA09M54964Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 294-W3-004 EXISTING REPAIR ON NR 4 SLAT L/H WING NOT ON MRCSSR NOR IS IT AN SRM REPAIR. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER IAW UPS E.O. MD11-5740-32607-AFeb 24, 2009 · N294UP · Doug MD11F · Leading Edge DevicesSDR IPXA09M54884Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 294-W3-010 IS NOT ON MRCSSR AND NOT PER SRM CUTOUT DOES NOT MEET MINIMUM REPAIR. REMOVED DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 7 VOL 1.Feb 24, 2009 · N294UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M54864Skin · damagedINSPECTION TYPE:1C REPAIR SURVEY SEQ 294-W4-04 RT WING FIXED L/E BETWEEN XIS 190-197 HAS AN EXISTING REPAIR WITH SINGLE ROW OF FASTENERS AROUND THE FLUSH REPAIR. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 VOL 1 FIGFeb 20, 2009 · N294UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M54841Repair · gougedINSPECTION TYPE:1C REPAIR SURVEY SEQ 294-W3-002 LT WING FIXED L/E UPPER SKIN BETWEEN XOS 452.1-467.1 PREVIOUS REPAIR IS GOUGED AT SLAT TRACK CUTOUT. REMOVED REPAIR, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 43.Feb 19, 2009 · N294UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M54902Doubler · crackedINSPECTION TYPE:1C RT WING FIXED L/E BEADED DOUBLER XFW 669 HAS 5 INCH CRACK. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW MD-11 SRM 57-10-00 FIG 27.Feb 17, 2009 · N294UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M54827Repair · gougedINSPECTION TYPE:1C REPAIR SURVEY SEQ F1-08, EXISTING REPAIR AT CTR CARGO DOOR CUTOUT, AFT LWR CORNER IS GOUGED. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER 3 EACH AND FILLER 4 EACH IAW MD-11 SRM 53-50-00 FIG 7.Feb 16, 2009 · N294UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS09M54800Repair · gougedINSPECTION TYPE:1C REPAIR SURVEY SEQ F1-04, EXISTING REPAIR AT FWD CARGO DOOR CUTOUT, AFT LWR EDGE IS GOUGED. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR REF MD11 SRM 53-50-00 FIG 17.Feb 16, 2009 · N294UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA09M54958Skin · dentedINSPECTION TYPE:1C TRANSFERRED FROM DMI-LOG D-379822: FUSELAGE SKIN DENT AT STA 798 RT ALTERNATE STATIC PORT. COLD FORMED DENT, FABRICATED AND INSTALLED INTERNAL REPAIR DOUBLER PER UPS EO MD11-5330-32591-A.Feb 15, 2009 · N294UP · Boeing · Fuselage Main, Plate/SkinSDR UPS09M54648Rudder · dentedINSPECTION TYPE:N/A RT UPPER RUDDER DENT. REPAIRED PER EO MD11-5540-31212-B.Feb 9, 2009 · N294UP · Doug MD11F · Rudder StructureSDR UPS08M52644Switch · inoperativeREF M379214, R1 PUSH-TO-TEST SWITCH INOP. COMPLIED WITH DMP 25-61-2 SLIDE PRESSURE GOOD. ITEM REMAINS ON DEFERRAL.Jul 3, 2008 · N294UP · Doug MD11F · Escape SlideSDR UPS08M52396Pump · leakingINSPECTION TYPE:N/A ATB - NR 2 HYDRAULIC FAIL ALERT MESSAGE. EMERGENCY DECLARED. FOUND NR 2 ENGINE L FWD HYD PUMP LEAKING FROM CASE DRAIN. REMOVED AND REPLACED NR 2 ENG LT & RT HYDRAULIC PUMPS AND FILTERS.May 31, 2008 · N294UP · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR UPS08M52150Fairing · damagedINSPECTION TYPE:C PYLON NR 2 EXHAUST FAIRING LT FWD SEAL MOUNT 3RD HOLE FROM BOTTOM FOUND ELONGATED AFTER REMOVAL OF SEAL AND RETAINER. DAMAGED AREA TRIMMED OUT PER EN1131-08. HFEC INSP C/OUT PER DAC NDTSPM R.13 06-10-01.001 FOUND NO CRACK EVIDENT. EXTERNALMar 20, 2008 · N294UP · Doug MD11 · Nacelle/Pylon Miscellaneous StructureSDR UPS08M52149Fairing · damagedINSPECTION TYPE:C PYLON NR 2 EXHAUST FAIRING RT FWD SEAL 2ND MOUNT HOLE FROM BOTTOM FOUND ELONGATED AFTER REMOVAL OF SEAL AND RETAINER. DAMAGED AREA TRIMMED OUT PER EN1131-08 AND MD11-54-20174. HFEC INSP C/OUT PER DAC NDT SPM R.13 06-10-01.001 FOUND NO CRACKMar 20, 2008 · N294UP · Doug MD11 · Nacelle/Pylon Miscellaneous StructureSDR UPS08M52134Longeron · crackedINSPECTION TYPE:C CTR CARGO COMPT BILGE AREA BETWEEN STA 1781 AND STA 1801 AT RT LONGERON 45 FOUND SUSPECTED CRACK. HFEC INSP C/OUT IAW DAC NDT SPM R.13 PART06-10-01.001 AND CRACK CONFIRM APPROX 1 1/4 INCH. CRACKED LONG REMOVED FR STA 1671-1811 L45 RT PER SRFeb 22, 2008 · N294UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52152Longeron · corrodedINSPECTION TYPE:C CTR CARGO BILGE AREA STA 1541 LONGERON R48 FOUND WITH CORROSION AS MARKED (DECAL 7932) LONGERON CORROSION REMOVED FOUND EXCEED LIMIT PER SRM 53-10-00 FIG 2A V OL1R.40 MATL REMOVED .118" ORIG THK:0.150". EXISTING SKIN STRAP REMOVED FR STA 5-9Feb 16, 2008 · N294UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52071Structure · corrodedINSPECTION TYPE:C CENTER CARGO BILGE RT L48 STA 1715-1695 FOUND MAJOR CORROSION ON LONGERON AS MARKED, LONGERON MAJOR CORROSION REMOVED. FOUND EXCEEDED LIMIT PER SRM 53-10-00 FIG 2A V.1R.40. MAT`L REMOVED:0.075 INCH ORIG THK:0.105 INCH. NEW LONG REWORK C/OUFeb 14, 2008 · N294UP · Doug MD11 · Fuselage Main, StructureSDR UPS08M52012Longeron · corrodedINSPECTION TYPE:C CENTER CARGO BILGE LH44 STA 1721 FOUND CORROSION AS MARKED ON LONGERON UNDERSIDE. LONGERON CORROSION REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-10-00 FIG 2A V.1R.40. MATL REMOVED:0.044", ORIG THK:0.071". CORRODED LONG SPLICE CUT C/OUT AT Feb 14, 2008 · N294UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52010Longeron · corrodedINSPECTION TYPE:C CENTER CARGO BILGE LT 46 STA 1721 FOUND CORROSION AS MARKED ON LONGERON STA 1721 L46 LT CORROSION REMOVED, REMOVED THK0.027" ORIG THK:0.072 INCH FOUND EXCEEDED LIMIT PER SRM 53-10-00 FIG 2A V.1R.40. CORRODED LONG SPLICE CUT C/OUT AT STA 1691Feb 14, 2008 · N294UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52055Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE PIVOT BORE HOLE AND FACE AREA FOUND RUSTY AS MARKED. (PIVOT BEARING REMOVED). LEFT FWD O/B FLAP I/B HINGE PIVOT BORE HOLE & FACE AREA CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08.Feb 13, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52030Skin · damagedINSPECTION TYPE:C LT WING FIXED L/E LOWER SURFACE ABOVE NR 1 ENGINE PYLON O/B SIDE AT APPROXIMATELY STA XORS 299 FOUND SCRATCH MARKS AS MARKED. DAMAGE SKIN REMOVED PER SRM 51-31-01V.2R.40. NEW SKIN FAB PER BOEING DRAWING ARB2363 USING MATL 7075T6-0.090". NEFeb 12, 2008 · N294UP · Doug MD11 · Wing, Plate/SkinSDR UPS08M52013Frame · crackedINSPECTION TYPE:C FAC AFT COMPARTMENT AT STA 449.250 FOUND CRACKED FRAME STRUCTURE JUST BELOW NR 1 RAM AIR INLET SCOOP AFT SECTION AS MARKED. DAMAGE AT RETURN FLANGE TRIM OFF PER EN1071-08. HFEC INSP C/OUT PER DAC NDTSPM R.13 PART06.10.01.001 FOUND NO CRACK Feb 12, 2008 · N294UP · Doug MD11 · Fuselage Main, FrameSDR UPS08M52136Frame · chafedINSPECTION TYPE:C RT RAM AIR EXHAUST CUTOUT FRAME STRUCTURE I/B FWD LOCATION FOUND DEEP CHAF CAUSED BY RAM AIR ACTUATOR LINKAGE. CHAFING MARK SMOOTHENED AND PROTECTED PER SRM 57-21-01V.2R.40. ORIG THK:0. 093 INCH, MATL REM:0.041" FOUND OUT OF LIMIT PER SRM 5Feb 11, 2008 · N294UP · Doug MD11 · Fuselage Main, FrameSDR UPS08M52084Spar · crackedINSPECTION TYPE:C LT WING FRONT SPAR ENCLOSURE APPROX STA XORS 514 UPPER SKIN FOUND CRACKED. CRACK AREA TRIM OFF PER EN1007-08. HFEC CARRIED OUT IAW DAC NDT SPM R.13 PART06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR ANGLES FAB USING 7075-0-0.063" MAT`L PER SRFeb 4, 2008 · N294UP · Doug MD11 · Wing SparSDR UPS08M52029Skin · corrodedINSPECTION TYPE:C RT I/B TE FLAP O/B LOWER SEGMENT BOTTOM SKIN TO BE REPLACED DUE TO MULTIPLE DENTS AND CORROSION. NEW SKIN FABRICATED PER BOEING DRAWING ARC2444 USING MATL 2024T3-0.040" NEW SKIN HOLES PICKED UP PER SRM 51-31-01 V.2R40. NEW SKIN PROTECTED PEFeb 3, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52028Skin · corrodedINSPECTION TYPE:C RT I/B TE FLAP LOWER SEGMENT BOTTOM SKIN TO BE REPLACED DUE TO MULTIPLE DENTS AND CORROSION. NEW SKIN FABRICATED PER BOEING DRAWING ARC2736 USING 2024T3-0.040" MATL NEW SKIN HOLE PICKED UP PER SRM 51-31-01 V.2R.40. NEW SKIN PROTECTED PER SRFeb 3, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M51971Longeron · crackedINSPECTION TYPE:C CAC: BETWEEN STA 6-70 AND STA 6-90, LONGERON 52L FOUND CORROSION CRACK. EXISTING LONG END SPLICE & LONG FASTENERS REMOVED AT STA 6.50-6.90 L52 PER SRM 51-31-01 V.2R.40. CORRODED LONG CUT OUT AT STA 6-60L52 PER SRM 53-10 00 FIG 1V.1R.40. HJan 31, 2008 · N294UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52139Seat Track · corrodedINSPECTION TYPE:C CABIN RT SEAT TRACK AT STA 1964-1953 RBL=107 FOUND CORRODED AS MARKED. CORRODED SEAT TRACK REMOVED PER SRM 51-31-01V.2R.40. HFEC INSP C/OUT IAW DAC NDTSPM 06-10-01.001R.13 FOUND NO CRACK EVIDENT. NEW SEAT TRACK AND SPLICE REWORK PER SRM 53Jan 30, 2008 · N294UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52085Skin · chafedINSPECTION TYPE:C RT I/B AILERON FOUND CHAFF MARKS ALONG L/E LOWER SKIN, O/B SIDE. RT I/B AILERON CHAFF SKIN REMOVED PER SRM 51-35-01 V.2R.40. NEW SKIN HOLES PICKED UP PER SRM 51-31-01V.2R.40. NEW SKIN INSTALLED PER SRM 51-35- 01V.2R.40. RHW I/B AILERON LOJan 27, 2008 · N294UP · Doug MD11 · AileronsSDR UPS08M51974Skin · chafedINSPECTION TYPE:C LEFT I/B AILERON FOUND CHAFE MARKS ALONG L/E LOWER SKIN I/B SIDE. CHAFED SKIN REMOVED PER SRM 51-35-01 V.2R40. HOLES ON NEW SKIN PICKED UP PER SRM 51-31-01 V.2 REV.40. NEW SKIN INSTALLED PER SRM 51-35-01 V.2 REV.40.Jan 27, 2008 · N294UP · Doug MD11 · Ailerons
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