N803DH

Service difficulty reports · 573

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 = 'N803DH' 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 DHLA201200003Blade · missingNR 1 ENGINE FAILED WHEN ENCOUNTER OF CAT AT FL 370 OCCURED. PERFORMED ENGINE FAILURE CHECKLIST AND INFLIGHT AIRSTART ABNORMAL PROCEDURE AND ENGINE SHUTDOWN PROCEDURE. ENGINE MOTORED FROM 0406 TO 0629. OIL PRESSURE AT FAILURE NORMAL, IN CRUISE 10 PSI. FUEL AJan 31, 2012 · N803DH · Doug DC873F · Turbine SectionSDR DHLA2012010600001Fire Detector · malfunctionedNR 3 ENGINE FIRE WARNING, PHASE ONES COMPLETED & ENGINE CHECKLIST, FIRED BOTTLE, LIGHT WENT OUT. OIL PRESSURE WAS POSITIVE. ACFT DIVERTED, ACFT WAS GROUNDED. INSPECTED ENGINE IAW MM 72-00-00. NO DEFECTS NOTED. INSPECTED ENGINE FOR EVIDENCE OF POSSIBLE FIREJan 6, 2012 · N803DH · Doug DC873F · Fire DetectionSDR DHLA201000143Seat Track · wornCOCKPIT.- F/E'S FWD SEAT TRACK HOLES ELONGATED. CORRECTIVE ACTION: REMOVED F/E'S FWD SEAT TRACK IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SEAT TRACK IAW SRM 51-3-0, SRM 51-3-1. OPS CHECKED GOOD IAW MMS 25-11-02 PG 501.Oct 29, 2010 · N803DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHLA201000144Frame · wornNR 4 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 202.000, BETWEEN 7 AND 8 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED AREA + FABRICATED FRAME SEGMENT (AL6061T6 0.071") IAW DWG EOct 26, 2010 · N803DH · Doug DC873F · Engine Thrust ReverserSDR DHLA201000090Battery Pack · failedEMERGENCY BATTERY WILL NOT TEST EXIT LIGHTS. ACFT WAS GROUNDED. R & R EMERGENCY EXIT LIGHT RACK ASSY. OPS CHECKS GOOD IAW MM 33-50-01.Sep 12, 2010 · N803DH · Doug DC873F · Emergency LightingSDR DHLA201000083Skin · corrodedNOSE SECTION LWR PLATING SHOWS CORROSION FS 12.000 L-36 PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 3,4,23,24. TR 53-203 DATED 01-21-08. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED AREA + FABRICATEJul 20, 2010 · N803DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000087Skin · corrodedSKIN CORRODED STA 520.000 L34R PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 07-16-10, EVA D853-00356 REV IR DATED 07-27-10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED AREA AND FABRICATED REPAIR DOUJul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000080Longeron Fitting · crackedLONGERON END FITTING BATHTUB FITTING CRACK 3.5" STA 902.125, L-4L PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED BATHTUB FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING IJul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHLA201000079Longeron Fitting · crackedLONGERON END FITTING BATHTUB FITTING CRACK 2.5" STA 902.125, L-5L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED BATHTUB FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING Jul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHLA201000076Skin · wornRIGHT INBD AILERON UPPER PLATING WORN STA XA 474.000 PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 1. REMOVED WORN PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-8-1 FIG. 1 ITEM "E". CLEANED, TREATED AND PRIMED AREA + NEWJul 8, 2010 · N803DH · Doug DC873F · AileronsSDR DHLA201000075Doubler · crackedNOSE SECTION ACCESS DOOR 2 INTERNAL DOUBLER CRACKED STA-156.0000. PERFORMED MAJOR REPAIR IAW EVA D853-00350, REV IR DATED 07-15-10. REMOVED EXISTING REPAIR IAW SRM 51-1-20D, SRM 51-1-21. VISUALLY INSPECTED REWORKED AREA. NO CRACK, NO CORROSION FOUND. FABRICATJul 8, 2010 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHLA201000072Splice · crackedFUS TAIL SECTION.- SPLICE FITTING CRACKED 1" STA 1766.00 L-17L PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED END FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW END FITTING IAW SRM 51-1-11Jul 8, 2010 · N803DH · Doug DC873F · Fuselage Main, StructureSDR DHLA201000084Splice · crackedAFT CARGO COMPT.- SPLICE FITTING CRACKED 6" (STA 1140.000 - 1160.000 L36) PERFORMED MAJOR REPAIR IAW JC EC-02172-001 W/O 9440. REMOVED SPLICE FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED, PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTINGJul 6, 2010 · N803DH · Doug DC873F · Fuselage Main, StructureSDR DHLA201000082Skin · corrodedLOWER FUSELAGE SKIN CORRODED STA 670.000 - 680.000, L36 - L35L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR10380 DATED 08-09-10, EVA D853-00355 REV IR DATED 07-19-10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOJul 6, 2010 · N803DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHLA201000078Cargo Track · wornUPPER CARGO COMPT.- NR 6 TRACK LUGS WORN (STA 560.000 - 610.000) PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG 14, SHEET 1, PG 49-50. REMOVED EXISTING SPLICES AND CUT OUT TRACK DAMAGED SEGMENT IAW SRM 53-2-3 FIG. 14 SHEET 1, SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATEDJul 6, 2010 · N803DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHLA201000073Rib · crackedRIGHT INBD FLAP T/E RIB CRACKED 1", STA XW -5.000 REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOPHOLE AND FABRICATED REPAIR ANGLE (AL2024T3 0.071") IAW SRM 57-2-0 PG 9-10, SRM 57-5-2 FIG. 5 SHEET 1, SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA + REPAJul 6, 2010 · N803DH · Doug DC873F · Trailing Edge FlapsSDR DHLA201000081Skin · damagedRT OTBD FLAP UPPER SKIN HOLE ELONGATED AND WORN STA XF 203.000 - 213.000 PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG 4, TR 57-94 ITEM Jul 2, 2010 · N803DH · Doug DC873F · Trailing Edge FlapsSDR DHLA201000077Longeron · crackedLONGERON 24R CRACKED 1.5" STA FS 900.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 5, SHEET 1, 13, 14, 15, 16, 25, 26, 27 TR 53-123 DATED 05-15-01. REMOVED FASTENERS IAW SRM 51-1-20D. PERFORMED STOP HOLE AND FABRICATED 2 REPAIR ANGLES, & 2 SHIMS IAW SRM 53-Jul 1, 2010 · N803DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHLA201000088Frame · wornNR3 ENG LT T/R FRAME WORN AT 6.30 AND 7.30 O'CLOCK POS STA YN 203.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-04-10, EVA D878-00353 REV IR DATED 07-15-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED AREA AND FABRICATED FRAME SEGMJun 30, 2010 · N803DH · Doug DC873F · Engine Thrust ReverserSDR DHLA201000085Skin · crackedRT WING TOP AFT PANEL PLATING CRACKED 4" STA XCW 69.500 PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 20, SHEET 1. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED AREA + FABRICATED (-5) DOUBLER (7075"0" 0.160") + (-7) TRIPLER (7075"0" 0.125") + FIJun 30, 2010 · N803DH · Doug DC873F · Wing, Plate/SkinSDR DHLA201000010Fire Warning · activatedAFTER TAKEOFF, NR 1 ENGINE FIRE WARNING. (USING "A" LOOP) PERFORMED EMERGENCY PROCEDURES, FIRED BOTH BOTTLES. WARNING CONTINUED AFTER LANDING, PENDING; ACFT IS GROUNDED.Apr 15, 2010 · N803DH · Doug DC873F · Fire DetectionSDR DHLA201000008Pump · low pressureNR 3 ENGINE AT FLT LEVEL 330 STARTED TO VIBRATE THEN DROPPED TO 70 PERCENT N1. MOVING THRUST LEVER HAD NO EFFECT. AFTER APPROX 1 MINUTE OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESS INDICATES 3 PSI. ENG SHUTDOWN PROCEDURE ACCOMPLISHED. T/S IAW MM 71-00-00 NOMar 18, 2010 · N803DH · Doug DC873 · Engine Fuel PumpSDR DHLA201000002Strut · leakingAFTER PUSH BACK, MX REPORTED LEAK FROM NOSE GEAR. RII ITEM. ACFT IS GROUNDED- REPLACING NOSE GEAR ASSY.Jan 7, 2010 · N803DH · Doug DC873 · Nose/Tail Landing Gear Strut/AxleSDR DHLA200800105Battery Pack · inoperativeEMERGENCY LIGHTS WILL NOT TEST ON PREFLT, ACFT GROUNDED. R&R BATTERY PACK ASSY, OPS CHECKED GOOD IAW 33-50-1.Sep 30, 2008 · N803DH · Doug DC873 · Emergency LightingSDR DHLA200800077Engine · failedAT TOP OF CLIMB NR 3 ENGINE FAILED FOLLOWED APPLICABLE PROCEDURES RELIGHT ATTEMPT UNSUCCESSFUL WIND MILLING OIL PRESSURE 2 PSI WIND MILLING TIME 2.55. PERFORMED T/S IAW DC8-70 M/M 71-00, ADJUSTED MEL SPECIFIC GRAVITY IAW MM 73-20-1. ADJUSTED PMC DROP IAW MM Jun 27, 2008 · N803DH · Doug DC873 · Engine (Turbine/Turboprop)SDR DHL2007803545Skin · delaminatedLT AFT ADF SENSE ANTENNA SKIN DELAMINATED. REMOVED AND REPLACED LT AFT ADF SENSE ANTENNA IAW SRM 51-3-0.Jun 14, 2007 · N803DH · Doug DC873 · Fuselage Main, Plate/SkinSDR DHL2007803537Skin · delaminatedRT WING T/E UPPER PANEL SKIN DELAMINATED (STA XW 0.000 - 47.000). REMOVED DELAMINATED PANEL IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-3-0, SRM 51-3-1 PG 2A (TORQUE).Jun 12, 2007 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007803542None · noneREMOVE REPAIR BELOW CARGO DOOR AT STA 176 AND INSPECT AREA. INSTALL A NEW REPAIR IAW SRM (PERMANENT) OR APPROVED DATA. ENTER INFORMATION ON 337 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-53-11 REV IR DATED 06-01-0Jun 10, 2007 · N803DH · Doug DC873 · Standard Practices/StructuresSDR DHL2007803543Frame · wornNR 3 ENG T/R FIXED STRUCTURE AND FWD FRAME WORN STA YN 202.000 AT 5 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3- DATED 06-08-07, DWG NR AD42-78-110 REV IR DATED 05-30-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION Jun 10, 2007 · N803DH · Doug DC873 · Nacelle/Pylon, Frame/Spar/RibSDR DHL2007803539Skin · wornNR 2 ENG NACELLE INLET COWL UPPER SIDE WORN, STA YN 147.534 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLICE 17.7 PJun 10, 2007 · N803DH · Doug DC873 · Nacelle/Pylon, Plate/SkinSDR DHL2007803541Skin · wornNR 1 ENG NACELLE INLET COWL UPPER SIDE WORN, STA YN 147.534 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLICE 17-7PH 0.Jun 10, 2007 · N803DH · Doug DC873 · Nacelle/Pylon, Plate/SkinSDR DHL2007803540Skin · wornNR 4 ENG NOSE COWL EXT SKIN WORN (STA YN 147.000 - 157.000 AT 12 O'CLOCK POS LT/RT) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND Jun 10, 2007 · N803DH · Doug DC873 · Nacelle/Pylon, Plate/SkinSDR DHL2007803538Skin · wornNR 3 ENG NOSE COWL EXTERNAL SKIN WORN (STA YN 147.534, AT 12 O'CLOCK POS) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLIJun 10, 2007 · N803DH · Doug DC873 · Nacelle/Pylon, Plate/SkinSDR DHL2007803536None · noneREMOVE REPAIR BELOW MAIN CARGO DOOR AT STA 226 AND INSPECT AREA. INSTALL NEW REPAIR IAW SRM (PERMANENT) AND APPROVED DATA. ENTER INFORMATION ON 337 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-08-07, DWG NR AD42-53-112 REV IR DATED 06-Jun 10, 2007 · N803DH · Doug DC873 · Standard Practices/StructuresSDR DHL2007803535Channel · wornRT MLG INBD DOOR ZEE CHANNEL WORN STA 870.000 RBL 50" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-52-0108 REV IR DATED 05-22-07. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATJun 8, 2007 · N803DH · Doug DC873 · Landing Gear DoorsSDR DHL2007803534Skin · wornRT OUTBD FLAP UPPER SKIN WORN, STA XF 224.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-57-106 REV IR DATED 05-21-07. REMOVED EXISTING REPAIR PLATING AND INNER DOUBLER IAW SRM 51-1-21. FABRICATED NEW PLATING SEGMJun 8, 2007 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007803533None · noneRT INBD VANE SLOT HAS AN INTERIM REPAIR AT STA XILD 42 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-2007, DWG NR AD42-57-107 REV IR DATED 05-21-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTIOJun 8, 2007 · N803DH · Doug DC873 · Standard Practices/StructuresSDR DHL2007803531Longeron · damagedFUS NOSE SECTION LONGERON HAS A MISDRILLED HOLE AT STA -32.000 L-17R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-04-07, DWG NR AD42-53-109 REV IR DATED 05-25-07. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REINFORCEMENT (AL7075T6 5Jun 6, 2007 · N803DH · Doug DC873 · Fuselage Main, Longeron/StringerSDR DHL2007803532Access Door · crackedLT FUS NOSE SECTION ACS MODIFICATION DOUBLER AT UPPER AFT JAMB CORNER OF HEAT EXCHANGER ACCESS DOOR, CRACKED 0.250" STA -12.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-04-07, DWG NR AD42-53-103 REV IR DATED 05-16-07. REMOVEDJun 6, 2007 · N803DH · Doug DC873 · DoorsSDR DHL2007803544None · nonePERFORM MODIFICATION REPAIR TO THE L2 DOOR, FWD, LOWER CORNER IAW AD2000-20-08, S/B 53-075 AND SR08530021. MAKE ENTRY IN AIRCRAFT LOGBOOK AND PERMANENT RECORD (337 FORM) MAJOR REPAIR (AMOC). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 05-22-07, BOEING MJun 5, 2007 · N803DH · Doug DC873 · Standard Practices/StructuresSDR DHL2007803526Doubler · crackedRT WING CTR L/E UPPER ANGLE DOUBLER CRACKED STA XFS 428.000. REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED ANGLE DOUBLER (AL7075"0" 0.080") IAW SRM 57-2-0 PG 9-10, SRM 57-3-3. HEAT TREATED ANGLE DOUBLER FROM 7075"0" TO 7075T6 IAW SJun 4, 2007 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007803523Vane · unknownLT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDO 67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-01-07, DWG NR AD42-57-105, REV IR DATED 05-17-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTIJun 3, 2007 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2007807524Vane · unknownRT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT SOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-01-07, DWG NR AD42-57-101 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTIONJun 3, 2007 · N803DH · Doug DC873 · Wing Main, Frame StructureSDR DHL2007803529Vane · unknownRT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDO 67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3- DATED 06-01-07, DWG NR AD42-57-102 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTIJun 3, 2007 · N803DH · Doug DC873 · Wing Main, Frame StructureSDR DHL2007803527Fitting · crackedNR 4 ALT TANK INTERIOR FITTING CRACKED 1" STA XW 408.000 S-58 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00363-001, DOUGLAS DWG NR 5644972. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. IJun 3, 2007 · N803DH · Doug DC873 · Wing, Attach FittingsSDR DHL2007803528Rib · crackedNR 4 STUB WING RIB CRACKED STA XOLDO 67.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00364-001, DOUGLAS DWG NR 9753297. REMOVED CRACKED RIB IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED Jun 3, 2007 · N803DH · Doug DC873 · Wing, Rib/BulkheadSDR DHL2007803530Vane · unknownLT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-01-07, DWG NR AD42-57-104 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECJun 3, 2007 · N803DH · Doug DC873 · Wing Main, Frame StructureSDR DHL2007803519Channel · crackedRT WING LWR FAIRING ZEE CHANNEL CRACKED 1" STA XW -3.125. REMOVED CRACKED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21. REFER TO JC EC-00360-00 (WO 1028) FOR ZEE FABRICATION.Jun 3, 2007 · N803DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2007803521Panel · crackedLT WING LWR PANEL CRACKED 1" STA XW -3.125. REMOVED PANEL IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-00359-001 (WO 1028) FOR PANEL FABRICATION.Jun 3, 2007 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007803520Channel · crackedLT WING LWR FAIRING ZEE CHANNEL CRACKED 0.750" STA XW -3.125. REMOVED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21. REFER TO JC EC-00361-001 (WO 1028) FOR ZEE FABRICATION.Jun 3, 2007 · N803DH · Doug DC873 · Wing Miscellaneous Structure
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