Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR IXXA09SMN53SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 717.000 LEFT BOTTOM LINE 1. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21, SRM 51-3-1.Apr 1, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN052SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT RUDDER SKIN CRACKED AT STATION ZR 71.437. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED RUDDER WEIGHT AND BAApr 1, 2009 · N605AL · Doug DC873F · Rudder, Plate/SkinSDR IPXA09855276Doubler · gougedINSPECTION TYPE:SV SURVEY SEQ 814-F1-55 EXTERNAL DOUBLER AT STA 11-18 BETWEEN LONGERON 1. 15L AND 16L HAS DEEP GOUGE. REPAIR ACCOMPLISHED PER REO-G12631 REV B AND UPS EO DC8-5320-32915A.Apr 1, 2009 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IPXA09855275Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 814-F1-10 EXTERIOR FUSELAGE DOUBLER AT BS 306 TO 312 HAS MINIMUM FASTENER SPACING LESS THAN 4D. ACCOMPLISHED REPAIR PER TIMCO REO-G12650 REV A AND UPS EO DC8-5320-328 04 REV A. DATE 3/20/09.Apr 1, 2009 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IPXA09855273Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 814-F1-16 DOES NOT CORRELATE TO A SRM REPAIR. REPAIR PER DC8 SRM 53-2-1 FIG 7 SHT 11 TR 53-703.Apr 1, 2009 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IPXA09855272Doubler · gougedINSPECTION TYPE:SV RT WING 51BD FLAP STA XF 225.740 REPAIR DOUBLER GOUGED SURVEY SEQ 81 4--W4-03. REPAIR ACCOMPLISHED PER TIMCO REO-G12584 REV IR AND UPS EO DC8-5720-32 210-A.Apr 1, 2009 · N814UP · Doug DC873F · Trailing Edge FlapsSDR IPXA09855271Structure · misrepairedINSPECTION TYPE:SV SURVEY SEQ 8114-F1-41 REPAIR DOUBLER AT STA 1712-1722 L17L-L18L DOES NOT CORRELATE TO SRM. REPAIR ACCOMPLISHED PER DC SRM 53-2-1 FIG 7 SHT 13 TR 53-203.Apr 1, 2009 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA09SMN063SCargo Track · wornDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK LUGS WORN AT STATION 1670.000-1752.000. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES. FABRICATED TRACK SEGMENT. CLEANED, TREATED, PRIMED AREA AND SEGMENT TRACK AND EXISTING SPMar 31, 2009 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA09SMN050SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CRACKED STATION 1260.000 - 1280.000 LONGERON 35 RIGHT. REMOVED CRACKED LONGERON. FABRICATED LONGERON, SPLICE, AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN049SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CRACKED STATION 1260.000 - 1280.000 LONGERON 35LEFT. REMOVED CRACKED LONGERON. FABRICATED LONGERON, SPLICE, AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLEDMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN051SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CRACKED AT STATION 1260.000 - 1280.000 LONGERON 36. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON SEGMENT EXTRUSION, SPLICE, AND DOUBLER. CLEANED, TREATED, PRIMED AREA ANDMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN048SLongeron · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CORRODED AT STATION 1490.000 - 1500.000 LONGERON 35 RIGHT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED LONGERON. FABRICATED LONGERON SEGMENT, AND SPLICES. PERFORMEDMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN047SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT LONGERON BATHTUB FITTING CRACKED AT STATION 902.125 LONGERON 5 LEFT. REMOVED CRACKED BATHTUB FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20D, SRM 51-1Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA90SMN046SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STATION 1230.000 LONGERON 32-33 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, AND SRM 51-3-1.Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN045SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE LONGERON CRACKED AT STATION 1786.000 LONGERON 17 LEFT. REMOVED CRACKED LONGERON. CLEANED, TREATED, AND PRIMED AREA. FABRICATED EXTRUSION LONGERON. INSTALLED REPAIR PART IAW SRM 53-5-3 FIGURE 5 SHEET 1 IMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN044SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE LONGERON CRACKED AT STATION 1786.000 LONGERON 17 RIGHT. REMOVED CRACKED LONGERON. CLEANED, TREATED, AND PRIMED AREA. FABRICATED EXTRUSION LONGERON. INSTALLED REPAIR PART IAW DC8 SRM 53-5-3 FIGURE 5 SHEEMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN042SStiffener · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 3 ENGINE THRUST REVERSER RIGHT COWLING RAIL FITTING CRACKED AT 6 O'CLOCK POSITION. REMOVED RAIL FITTING FASTENERS. FABRICATED NEW STIFFENER. PROTECTED STIFFENER WITH CHROMIC ANODIZED. INSTALLED NEW FASTENERS,Mar 30, 2009 · N605AL · Doug DC873F · Engine Thrust ReverserSDR IXXA09SMN041SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74.000 STRINGER 12. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORRMar 30, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA09SMN061SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT LEFT CAP CRACKED STATION 55.000 - 70.000 RIGHT BOTTOM LINE 45. REMOVED CRACKED CAP. INSTALLED NEW CAP IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND SMN-FOMar 30, 2009 · N605AL · Doug DC873F · Fuselage Main, StructureSDR IXXA09SMN060SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT LEFT CAP CRACKED STATION 55.000 - 70.000 LEFT BOTTOM LINE 45. REMOVED CRACKED CAP. INSTALLED NEW CAP IAW DC8 SRM 51-1-20D, SRM 51-3-1, REPAIR SPECIFICATION NR 2003-05, AND SMN-FORM-07 IPMar 30, 2009 · N605AL · Doug DC873F · Fuselage Main, StructureSDR IXXA09SMN039SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP INTERIOR FITTING CRACKED AT STATION XF 337.000. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-21, ATI REPAIR SMar 30, 2009 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA09SMN043SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER FRONT SPAR LOWER FITTING CRACKED AT STATION XFS 60.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.Mar 30, 2009 · N605AL · Doug DC873F · Horizontal Stabilizer, Attach FittingsSDR IXXA09SMN040SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP INTERIOR HAS FITTING CRACKED AT STATION XF 411.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-3-1, SRM 51-1-21.Mar 30, 2009 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA09SMN036SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN CRACKED AT STATION 104.000 - 122.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED REPAIR PART IAW SRM 57-7-1 FIGURE 1 ITEM "D",Mar 28, 2009 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IPXA09855185Doubler · gougedINSPECTION TYPE:SV RT WING L/E STA XFS 284 REPAIR DOUBLER GOUGED SURVEY 814-W4-18. INSTALLED REPAIR PER DC8 SRM 52-02-01-0 FIG 38 SHT 1.Mar 28, 2009 · N814UP · Doug DC873F · Wing, Plate/SkinSDR IPXA09855184Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 814-F1-46 DOUBLER STA 1282-1293 L33L-L34L. DOES NOT CORRELATE TO A SRM REPAIR. INSTALLED REPAIR PER DC8 SRM 53-2-1 FIG 7 SHT 13 TR 53-203 REV 78.Mar 28, 2009 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IPXA09855183Support Angle · damagedINSPECTION TYPE:SV CUSP SUPPORT ANGLE BETWEEN STA 1600 TO 1620 RBL 60 HAS DRILL DAMAGE ON SUB FLOOR LEG. INSTALL REPAIR PER DAC DWG 9750448.Mar 28, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA09SMN034SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE NOSE SECTION EXTERIOR PRIMARY HEAT EXCHANGER AFT LOWER CORNER CRACKED AT STATION 12.000 LONGERON 27 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CMar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, StructureSDR IXXA09SMN033SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE NOSE SECTION EXTERIOR PRIMARY HEAT EXCHANGER AFT LOWER CORNER CRACKED AT STATION 12.000 LONGERON 27 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRMar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, StructureSDR IXXA09SMN038SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT PASSENGER DOOR FITTING CRACKED AT STATION 1621.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1.Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN037SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 781.500 LONGERON 13 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D DC8 SRM 51-1-8B, AND SRM 51-3-1.Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN035SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 680.000 LONGERON 11 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-23, SRM 51-1-20D, DC8 SRM 51-1-8B, AND SRM 51-3-Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN032SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERIOR LOWER SKIN CORRODED AT STATION 660.000 LONGERON 31 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED AMar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA09SMN030SStructure · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON MAIN CARGO DOOR FORWARD LOWER JAMB CORNER AT STATION 120.000 - 210.000 LONGERON 19-23 LT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. Mar 26, 2009 · N605AL · Doug DC873F · Cargo/Baggage DoorsSDR IPXA09855173Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 752-W3-2 MINIMUM EDGE DISTANCE LESS THAN 1.5 ON REPAIR LT AUX FUEL TANK LOWER EDGE AT XFS 154. *SDR FILED OPEN*Mar 26, 2009 · N814UP · Doug DC873F · Wing, Plate/SkinSDR IXXA09SMN027SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT FUSELAGE SKIN FORWARD OF FLAT AFT PRESSURE BULKHEAD HAS IMPROPER REPAIR AT LONGERON 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, EXTERNAMar 21, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IPXA09855116Attach Angle · crackedINSPECTION TYPE:SV LEFT I/B FLAP SURFBOARD ATTACH ANGLE HAS TWO ADJACENT HOLES CRACKED OUT. ACCOMPLISHED REPAIR PER DC8 SRM 57-2-0 FIG 2A SHT 1 AND 57-2-0 SHT 2.Mar 21, 2009 · N814UP · Doug DC873F · Trailing Edge FlapsSDR DHLA200900017Line · crackedNR 4 OIL QUANTITY WENT TO 0 AND OIL 8 PSI ADHERED TO EMERGENCY PROCEDURE. FOUND OIL LINE TO ENG OIL PRESSURE XMITER CRACKED. REMOVED AND REPLACED LINE. OPS AND LK CHECK GOOD PER MM-79-32-1. SERVICED ENG OIL PER 12-20-1. RUN ENG, PER JRH CH 11 LINE ASSY P/Mar 19, 2009 · N807DH · Doug DC873F · Engine Oil Indicating SystemSDR DHLA2009805302Link · crackedRIGHT WING AT STATION XW97 FLAP DRIVE LINK ASSY HAVE CRACK AT ACTUATOR HOOK UP END.Mar 2, 2009 · N805DH · Doug DC873F · Trailing Edge Flap Control SystemSDR IPXA09854879Door · missingINSPECTION TYPE:N/A CLIMBING THROUGH 270FT, HEARD LOW THUMP, CABIN CLIMBED TO 18,000FT. RAN CABIN ALT WARNING CHECK LIST. COULD NOT MAINTAIN CABIN. DESCENDED TO 10,000FT. EMERGENCY DECLARED. FOUND GROUND CONDITIONED AIR DOOR ASSEMBLY MISSING FROM LOWER RIFeb 28, 2009 · N810UP · Doug DC873F · Cabin Pressure Control SystemSDR IPXA09855517Skin · misrepairedINSPECTION TYPE:SV SS 814-F1-40, FUSE EXT SURFACE SKIN FS 1740-1747, L16L-L17L, EXISTING REPAIR DOUBLER NOT EXTENDING ONE ROW OF FASTENERS PAST LONGERON. ACCOMPLISHED REPAIR PER TIMCO REO-G12721 REV B AND UPS EO DC8-5320-330 64A.Feb 20, 2009 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IPXA09855496Skin · misrepairedINSPECTION TYPE:SV SS 814-F1-09, WINDOW BELT REPAIR DOUBLER DOES NOT CORRELATE TO A SRM WITH THE RESPECT TO SIZE AND DIMENSION FS 200 TO FS 300 L15R-L17R. REPAIRED PER TIMCO REO-G12657 REV E, AND UPS EO DC8 5320-32976A.Feb 19, 2009 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IPXA09855492Skin · misrepairedINSPECTION TYPE:SV SS 814-F1-28, FUSELAGE WINDOW BELT DOUBLER, FS 1480-FS 1500, L15R-L17R DOES NOT CORRELATE TO A SRM WITH RESPECT TO SIZE AND DIMENSION. ACCOMPLISH REPAIR PER TIMCO REO-G12655 REV E, AND PER UPS EO DC8-5320 -32974A.Feb 19, 2009 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IPXA09855973Frame · crackedINSPECTION TYPE:SV CRACKED FORMER AT RT WING LE STA XFS 303 BOTTOM AFT. FABRICATED NEW FORMER AND INSTALLED PER DAC DWG 5769530 REV F, AND DC8 SRM 51-1-20D REV 78.Feb 18, 2009 · N852UP · Doug DC873F · Wing SparSDR IPXA09855721Skin · misrepairedINSPECTION TYPE:SV SS 852-F1-46, REPAIR DOES NOT CORRELATE TO A SRM, FS 92 - FS 100, L20R - L21R. ACCOMPLISHED THE FOLLOWING: ADDED ADDITIONAL FASTENERS REQUIRED BY DC8-SRM 53-2-1 FIG 7 SHT 15 AND TR 53-203.Feb 18, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IPXA09856125Skin · misrepairedINSPECTION TYPE:SV SS 852-W4-24, RT O/B FLAP LOWER SKIN REPAIR AT XF 215, DOES NOT HAVE .5 MINIMUM CORNER. REPAIRED PER TIMCO REO-G12754 REV B, AND UPS DC8-5750-33544-A.Feb 17, 2009 · N852UP · Doug DC873F · Trailing Edge FlapsSDR IPXA09856130Skin · misrepairedINSPECTION TYPE:SV SS 852-F1-39, REPAIR DOES NOT CORRELATE TO A SRM, NO FASTENER CALL OUT FOR DOUBLER THICKNESS FS 351-FS 368, L18R-L21R. REPAIRED PER REO-G12770 REV C, AND UPS DC8-5330-33639-A.Feb 16, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IPXA09855714Skin · misrepairedINSPECTION TYPE:SV SS 852-F1-30, REPAIR CONFIGURATION DOESN'T CORRELATE TO A SRM. DOUBLER TOO THICK. FS 1733.5 BETWEEN L28R AND L29R. REMOVED AND REPLACED DOUBLER PER DC8 SRM 53-2-1 FIG 7 SHT 15 AND TR 53-2 03.Feb 16, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA090005OTube · cloggedDURING DESCENT INTO ETAR NUMBER 2 ENGINE FLAME OUT. WITH THROTTLE REDUCTION, MILD VIBRATION, AND FUEL FLUCTUATION. THE CREW LANDED IN ETAR WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED CFM TROUBLESHOOTING TREE FAULT 51 AND FOUND CDP TUBES CLOGGED. MAIFeb 16, 2009 · N606AL · Doug DC873F · Fuel Control/Turbine EnginesSDR IPXA09855979Skin · dentedINSPECTION TYPE:SV SS NR 852-S4-08, LT SIDE, FLUSH REPAIR, STA ZR 170.656 HAS A DENT, GOUGED, TOOLING DAMAGE, AND FASTENERS DISTANCE LESS THAN 4D. REPAIRED PER TIMCO REO-G12807 REV IR, AND UPS EO NR DC8-5520-33390-A.Feb 15, 2009 · N852UP · Doug DC873F · Leading Edge Devices
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