# Service difficulty reports: Douglas DC-10-30F

A list on [Douglas DC-10-30F](https://openairdocs.org/model/douglas-dc-10-30f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 24 · 1,152 reports

- [SDR 2019F00027](https://openairdocs.org/sdr/2019F00027.md): Slide Raft · defective · May 21, 2018 · Doug DC1030F · Escape Slide
  > AIRCRAFT DECLARED AN IFE FOR SMOKE IN THE COCKPIT. UPON LANDING CREW DEPLOYED THE LEFT FORWARD DOOR (DOOR 1L) SLIDE/RAFT BUT IT FAILED TO FULLY INFLATE. FLIGHT CREW WENT TO DEPLOY THE SLIDE/RAFT LOCATED IN THE NUMBER 1 RIGHT DOOR (DOOR 1R) THE SLIDE/RAFT FEL
- [SDR FDEA201708222473](https://openairdocs.org/sdr/FDEA201708222473.md): Channel · chafed · Aug 22, 2017 · N307FE · Doug DC1030F · Vertical Stabilizer Miscellaneous Structure
  > LWR RT NR 2 ENG FAN COWL & IDG SHOW DEEP CHAFED IN STRUCTURE. TAPE/RED MARK REPAIRED AJC7415-6 CHAFED SECTION REF 55-00-01 FIG 7 SH 1-4 PG 25-28 VOL I.
- [SDR CA151123011](https://openairdocs.org/sdr/CA151123011.md): Circuit Breaker · faulty · Nov 22, 2015 · Doug DC1030F · AC Power Distribution System
  > (CAN) IN FLIGHT, THE AIRCRAFT EXPERIENCED A LT EMERGENCY AC BUSS ELECTRICAL FAILURE. THE FLIGHT CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST PROCEDURES AND DECLARED AN EMERGENCY, DIVERTED AND LANDED UNEVENTFULLY. THE MAINTENANCE INSPECTION FOUND A REMOTE CONTRO
- [SDR CA150303009](https://openairdocs.org/sdr/CA150303009.md): Thrust Reverser · damaged · Feb 17, 2015 · Doug DC1030F · Engine Thrust Reverser
  > (CAN) AFTER LANDING, THE FLIGHT CREW NOTICED THE NR 2 ENGINE THRUST REVERSER PRESSURE AND UNLOCK LIGHT REMAINED ILLUMINATED AFTER BEING SELECTED TO CLOSE. UPON INSPECTION, MAINTENANCE DETERMINED THE RT THRUST REVERSER ASSY WAS DAMAGED AND STUCK IN THE DEPLOYE
- [SDR CA150212009](https://openairdocs.org/sdr/CA150212009.md): Dimmer · failed · Feb 11, 2015 · Doug DC1030F · Instrument Panel
  > (CAN) IN FLIGHT, THE FLIGHT CREW NOTICED SMOKE EMITTING FROM THE COCKPIT OVERHEAD PANEL. THE ELECTRICAL SMOKE PROCEDURE CHECKLIST WAS CARRIED OUT AND THE SMOKE CEASED. THE CREW COMPLETED A FUEL DUMP BEFORE RETURNING TO BASE FOR AN UNEVENTFUL LANDING. MAINTENAN
- [SDR CA141208005](https://openairdocs.org/sdr/CA141208005.md): Switch · intermittent · Dec 5, 2014 · Doug DC1030F · Engine Oil Indicating System
  > (CAN) AT TOP OF CLIMB, THE NR 2 ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. CREW COMPLETED THE INFLIGHT SHUT DOWN PROCEDURE. AFTER LANDING SAFELY, THE OIL STRAINER FILTER WAS REMOVED/INSPECTED AND WAS FOUND CLEAN AND WITHOUT ANY CONTAMINATION. OIL STRAINER
- [SDR CA140321017](https://openairdocs.org/sdr/CA140321017.md): Line · split · Mar 17, 2014 · Doug DC1030F · Turbine Engine Oil System
  > (CAN) THE NR 3 ENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE CAUSED BY OIL DEPLETION. THE FLIGHT CONTINUED TO THE NEAREST SUITABLE AIRPORT WHERE MAINTENANCE DISCOVERED A RETURN OIL SCAVENGE LINE SPLIT AND LEAKING. FURTHER INVESTIGATION IDENTIFIED VIBR
- [SDR CA131218026](https://openairdocs.org/sdr/CA131218026.md): Control Handle · sticking · Dec 13, 2013 · Doug DC1030F · Landing Gear Selector
  > (CAN) ON APPROACH, AFTER EXTENDING THE GEAR THE FLT DECK INDICATION FOR THE GEAR, GREEN, FAILED TO ILLUMINATE ON BOTH THE FRONT AND REAR PANELS, ONLY THE RED UNSAFE LIGHTS ILLUMINATED. THE CREW CYCLED THE GEAR WITH THE SAME RESULT, SO THEY COMPLETED A MISSED
- [SDR CA130405007](https://openairdocs.org/sdr/CA130405007.md): Wheel Half · cracked · Apr 3, 2013 · Doug DC1030F · Wheel/Ski/Float
  > (CAN) 0.700" LONG CRACK FOUND ON OTBD WHEEL HALF DURING ROUTINE O/H PROCEDURES. METHOD USED TO DETECT CRACK WAS HFEC. CRACK ORIGINATES ON MATING SURFACE, BETWEEN SPOKE AND BOLT HOLE.
- [SDR FDEA201211063883](https://openairdocs.org/sdr/FDEA201211063883.md): Skin · dented · Nov 6, 2012 · N318FE · Doug DC1030F · Wing, Plate/Skin
  > LT OTBD FLAP BOTTOM SKIN HAS A CLUSTER OF SHARP DENTS JUST INBD OF VANE ROLLER ACCESS PANEL 557DB. INSPECTED DAMAGE AREA FOUND TO BE SERIES OF GOUGE SHARP CREASE DENTS TO INCLUDE ONE LOSE FASTENER - OUT OF LIMITS IAW SRM 57-10-00 PG 162A TO 48, HFEC DENT IAW
- [SDR CA130702005](https://openairdocs.org/sdr/CA130702005.md): Acm · failed · Mar 19, 2012 · Doug DC1030F · Cabin Cooling System
  > (CAN) NR 1 ACM COOLING TURBINE WHEEL SHAFT FAILED DURING GROUND RUNS, TURBINE EXITED ACFT THROUGH EXHAUST DOOR. THE ACM WAS REPLACED AND THE ACFT RETURNED TO SERVICE.
- [SDR FDEA201103261187](https://openairdocs.org/sdr/FDEA201103261187.md): Switch · failed · Mar 26, 2011 · N320FE · Doug DC1030F · Engine Oil Indicating System
  > ON INITIAL CLIMBOUT, RECEIVED ENG 2 OIL FILTER ALERT. USED MIN IDLE POWER AS ALERT WENT ON AND OFF SEVERAL TIMES FOR SEVEAL MINUTES EVENTUALLY REMAINED ON STEADY AT MIN IDLE. RED TABS FOR ALERT SHUTDOWN NR 2 ENGINE, RETURN TO DEPARTURE. NO OTHER ABNORMAL EN
- [SDR FDEA201007212632](https://openairdocs.org/sdr/FDEA201007212632.md): Door Frame · cracked · Jul 21, 2010 · N320FE · Doug DC1030F · Fuselage Main, Structure
  > MAIN CABIN CRACK ON WEB L3 DOOR LOWER JAMB AT STA 1251 REPAIRED IAW SRM 53-50-00 FIG 19, SH 1, VOL 1.
- [SDR FDEA201006252146](https://openairdocs.org/sdr/FDEA201006252146.md): Skin · gouged · Jun 25, 2010 · N315FE · Doug DC1030F · Fuselage Main, Plate/Skin
  > EXISTING GOUGE IN FUSELAGE SKIN ADJACENT TO NOSE JACK POINT ALIGNMENT HOLE REPAIRED IAW EA 8-5330-123164.
- [SDR CA100528012](https://openairdocs.org/sdr/CA100528012.md): Bolt · corroded · May 28, 2010 · Doug DC1030F · Engine Mount Section
  > DURING A RECENT SCHEDULED MX CHECK AND NR 2 ENGINE CHANGE PERSONNEL NOTICED EXCESSIVE PLAY AT THE TAIL PYLON THRUST LINK ASSY, PN AVB7320-501, LOWER ATTACHMENT. FURTHER INVESTIGATION IDENTIFIED THAT THE ATTACH BOLT, PN RA11005-12-2, WAS WORN AND CORRODED. NE
- [SDR FDEA201005071481](https://openairdocs.org/sdr/FDEA201005071481.md): Sill · corroded · May 7, 2010 · N320FE · Doug DC1030F · Fuselage Miscellaneous Structure
  > MODERATE CORROSION ON INTERIOR STRUCTURE OF LOWER AFT CARGO COMPT DOOR SILL. REPAIRED IAW EA 8-5310-123168 AND SRM 53-50-00 FIG.22, FIG.1, FIG.9, FIG.15A VOL.1.
- [SDR 22AA201000070](https://openairdocs.org/sdr/22AA201000070.md): Proximity Switch · inoperative · May 3, 2010 · N478CT · Doug DC1030F · Landing Gear Position and Warning
  > AFTER TAKEOFF WITH GEAR HANDLE UP ALL (4) RED UNSAFE LIGHTS REMAINED ILLUMINATED. COMPLETED APPROPIATED CHECK LIST, NO CHANGE IN THE LIGHTS INDICATION. NOTIFIED ATC, FLIGHT CONTROL AND MX CONTROL. RETURNED TO DEPARTURE. IAW TAFI 32-30-00, R & R PROXIMITY ELECT
- [SDR FDEA201004291395](https://openairdocs.org/sdr/FDEA201004291395.md): Skin · worn · Apr 29, 2010 · N315FE · Doug DC1030F · Wing, Plate/Skin
  > RT WING L/E DROOPED EXT FOUND DEEP WEAR ON SKIN. REPAIRED AREA IAW SRM 57-10-00, VOL I, FIG 39.
- [SDR FDEA201004261362](https://openairdocs.org/sdr/FDEA201004261362.md): Relay · malfunctioned · Apr 26, 2010 · N321FE · Doug DC1030F · Pneumatic Indicating System
  > AFTER TAKEOFF, ENG ANTI-ICE ON, RECEIVED AIR SYS 2 LEVEL 1 ALERT. 45 SECS LATER RECEIVED MANF 2 FAIL LEVEL 3 ALERT. COMPLIED WITH QRH & DIVERTED. AFTER 4 MINS WITH NR 2 ENG AT IDLE, LEVEL 3 ALERT OUT. RELEASED FOR SERVICE IAW MEL: 36-23-01-02. ON MANF FAIL D
- [SDR FDEA201004211265](https://openairdocs.org/sdr/FDEA201004211265.md): Longeron · corroded · Apr 21, 2010 · N320FE · Doug DC1030F · Fuselage Main, Longeron/Stringer
  > LT WING UPPER SIDE WING TO FUSELAGE FILLETS. AFTER REMOVING THE FILLETS 151 FT AND 151 ET WITH NRC NR N00866 THE FOLLOWING DEFECT HAVE BEEN FOUND EXFOLIATION CORROSION ON LONGERON. PERFORMED REPAIR IAW E.A. 8-5310-137606
- [SDR FDEA201004131170](https://openairdocs.org/sdr/FDEA201004131170.md): Panel · delaminated · Apr 13, 2010 · N320FE · Doug DC1030F · Wing, Plate/Skin
  > RT WING UPPER SURFACE T/E. REMOVING WING PANEL ARC0340-504 WITH N00458. FOUND DELAMINATION ON AFT EDGE. (REMOVED PART). REPAIRED DELAMINATION IAW SRM 51-71-00 PAR.16 VOL.2
- [SDR FDEA201003190931](https://openairdocs.org/sdr/FDEA201003190931.md): Skin · corroded · Mar 19, 2010 · N320FE · Doug DC1030F · Fuselage Main, Plate/Skin
  > CTR CARGO COMPT BILGE, 2 EA U/S ANCHOR PLATE ON SKIN. DURING ANCHOR PLATE REPLACEMENT FOUND CORROSION ON SKIN. REPAIRED SKIN IAW SRM 53-20-00 FIG.13 SH.6 VOL.1.
- [SDR FDEA201003090704](https://openairdocs.org/sdr/FDEA201003090704.md): Web · cracked · Mar 9, 2010 · N320FE · Doug DC1030F · Fuselage Miscellaneous Structure
  > COCKPIT AREA FOUND CRACKS ON WEB. REPAIRED CRACK IAW SRM 53-00-01, FIG 4, SHT 2, VOL I.
- [SDR FDEA201003040649](https://openairdocs.org/sdr/FDEA201003040649.md): Warning Light · illuminated · Mar 4, 2010 · N314FE · Doug DC1030F · Central Warning
  > AT CRUISE ALTITUDE 350, RECEIVED LEVEL 3 ALERT "AIR MANF 2 FAIL" COMPLIED WITH QRH AND PROCEEDED TO NEAREST SUITABLE KOKC FOUND SYSTEM TEST GOOD PER AMM 36-23-01-4.AS PRECAUTIONARY PERFORMED DECAY CHECK ON ALL 3 MANIFOLDS PER AMM 36-00-01-5.ALL MANIFOLDS
- [SDR 22AA201000066](https://openairdocs.org/sdr/22AA201000066.md): Skin · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK, LOWER FUSELAGE, ALONG LONGERON 44L, ALONG STA 1701 FUSELAGE SKIN FOUND CRACKED THROUGH. NON-ROUTINE NR 0425, CRACK AREA AT LONGERON 44L ALONG STATION 1701 FUSELAGE SKIN REPAIRED IAW SRM 53-20-00 FIGURE 6 VOLUME I REVISION 96.
- [SDR 22AA201000065](https://openairdocs.org/sdr/22AA201000065.md): Roller Tray · corroded · Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Floor Panel
  > DURING "C" CHECK, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY FOUND CORRODED AFTER CARGO SIDE GUIDE RAIL REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1697 TO STA 1781. NON-ROUTINE NR 0450, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY REPAIR CARRIE
- [SDR 22AA201000064](https://openairdocs.org/sdr/22AA201000064.md): Seat Track · corroded · Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage, Seat/Cargo Attach Fittings
  > DURING "C" CHECK, CABIN CORROSION FOUND ON INNER SURFACE OF SEAT TRACK AT STATION 1139 TO STATION 1156, X= 47.5. NON-ROUTINE NR 0314, SEAT TRACK FROM STATION 1129 TO STATION 1169, X= 47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIGURE 1 VOLUME 1 REVISION 96.
- [SDR 22AA201000063](https://openairdocs.org/sdr/22AA201000063.md): Intercostal · corroded · Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Miscellaneous Structure
  > DURING "C" CHECK, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL FOUND CORRODED AFTER SIDE GUIDE RAIL, REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1764, L42 TO L43L (REFER CNTRL NR 0425). NON-ROUTINE NR 0449, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL REPAIR
- [SDR 22AA201000062](https://openairdocs.org/sdr/22AA201000062.md): Skin · corroded · Feb 24, 2010 · N478CT · Doug DC1030F · Wing, Center Box
  > DURING "C" CHECK, CABIN CORROSION FOUND ON CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT). NON-ROUTINE 0220, CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT) CORROSION REMOVED AND REPROTECTED IAW SRM 51-21-01 VOLUME II AT S 21 F
- [SDR 22AA201000061](https://openairdocs.org/sdr/22AA201000061.md): Rib · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/Rib
  > DURING "C" CHECK, NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0297, CRACK AREA AT NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000060](https://openairdocs.org/sdr/22AA201000060.md): Rib · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/Rib
  > DURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0296, CRACK AREA AT NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000059](https://openairdocs.org/sdr/22AA201000059.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0202, CRACKED UPPER LONGERON AT NR 2 ENGINE RT CORE COWL AREA REPAIRED IAW 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FROM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000057](https://openairdocs.org/sdr/22AA201000057.md): Skin · worn · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Plate/Skin
  > DURING "C" CHECK, NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP FOUND WORN TO COWLING SKIN. NON-ROUTINE NR 0198, WORN COWLING SKIN AREA AT NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED
- [SDR 22AA201000056](https://openairdocs.org/sdr/22AA201000056.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 2 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0197, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000055](https://openairdocs.org/sdr/22AA201000055.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 2 ENGINE LT CORE COWL LOWER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0196, CRACK AREA AT NR 2 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000054](https://openairdocs.org/sdr/22AA201000054.md): Rib · worn · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/Rib
  > DURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0195, WORN AREA AT NR 2 ENGINE LT CORE COWL AFT MOST RIB AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000053](https://openairdocs.org/sdr/22AA201000053.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 3 ENGINE RT CORE COWL LOWER LONGERON CRACKED AT APPROX AT MID AND AFT FRAME SECTION. NON-ROUTINE NR 0163, CRACK AREA AT MID AND AFT SECTION OF LOWER LONGERON AT NR 3 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND F
- [SDR 22AA201000052](https://openairdocs.org/sdr/22AA201000052.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION FOUND CRACKED. NON-ROUTINE NR 0159, CRACK AREA AT NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2
- [SDR 22AA201000051](https://openairdocs.org/sdr/22AA201000051.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 1 ENG, RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 0125, CRACKED STRAP AND LOWER LONGERON AT NR 1 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000050](https://openairdocs.org/sdr/22AA201000050.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 1 ENG LT CORE COWL LOWER LONGERON FOUND CRACKED. NON-ROUTINE NR 0124, CRACK AREA AT NR 1 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR 22AA201000049](https://openairdocs.org/sdr/22AA201000049.md): Longeron · cracked · Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND CRACK. NON-ROUTINE NR 0123, CRACK AREA AT NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIR IAW EN 1016-10 AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
- [SDR FDEA201002230494](https://openairdocs.org/sdr/FDEA201002230494.md): Clamp · loose · Feb 23, 2010 · N314FE · Doug DC1030F · Compressor Bleed Control
  > BASED ON MX REPORT, DECIDED TO GIVE A LITTLE EXTRA TIME FOR ACCELERATION. IT WAS NECESSARY TO GO FULL QUADRANT TO GET CLOSE TO TAKEOFF POWER. WHEN THE AUTOFLIGHT TILE WAS PRESSED ENG 1 AND 2 REACHED TAKEOFF POWER, ENG NR 3 WAS LAGGING ABOUT 15 PERCENT BELOW
- [SDR FDEA201002180447](https://openairdocs.org/sdr/FDEA201002180447.md): Skin · dented · Feb 18, 2010 · N320FE · Doug DC1030F · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB EXTERIOR SURFACE FOUND DEEP NICK ON SKIN. (REMOVED PART). REPAIRED EDGE FWD SKIN IAW SRM 55-10-00 FIG.13 VOL.1, REPAIRED LEADING REAR SKIN IAW SRM 55-00-01 FIG.3 SH.2 VOL.1
- [SDR FDEA201002180448](https://openairdocs.org/sdr/FDEA201002180448.md): Skin · worn · Feb 18, 2010 · N315FE · Doug DC1030F · Wing, Plate/Skin
  > LT WING L/E DEEP WEARS & 4 EA FASTENERS U/S ON LOWER SKIN. REPAIRED AREA IAW EA 8-5710-137482 & SRM 57-10-00 FIG 83, VOL I.
- [SDR FDEA201002150426](https://openairdocs.org/sdr/FDEA201002150426.md): Skin · cracked · Feb 15, 2010 · N315FE · Doug DC1030F · Trailing Edge Flaps
  > LT WING INBD FLAP UPPER SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, SHT 2 & 4 VOL I.
- [SDR 22AA201000048](https://openairdocs.org/sdr/22AA201000048.md): Frame · corroded · Feb 13, 2010 · N524MD · Doug DC1030F · Fuselage Main, Frame
  > DURING "C" CHECK, AFT CARGO COMPARTMENT BILGE AREA FRAME (STA 1996) LOWER CHORD CORRODED AT LBL 15 TO RBL 15 AS MARKED. NON-ROUTINE NR 0610, AFT CARGO COMPARTMENT BILGE AREA FRAME (STA 1996) LOWER CHORD, LBL 15 TO RBL 15 CORROSION, REMOVED AND REPROTECTED IAW
- [SDR 22AA201000047](https://openairdocs.org/sdr/22AA201000047.md): Longeron · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 2 ENG RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 394, CRACKED LONGERON AND STRAP AT NR 2 ENG RT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.
- [SDR 22AA201000046](https://openairdocs.org/sdr/22AA201000046.md): Longeron · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK AT 02 LOCATIONS. NON-ROUTINE NR 392, CRACKED LONGERON 02 EACH LOCATIONS AT NR 2 ENGINE RT CORE COWL UPPER AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.
- [SDR 22AA201000045](https://openairdocs.org/sdr/22AA201000045.md): Longeron · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 324, CRACKED NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.
- [SDR 22AA201000044](https://openairdocs.org/sdr/22AA201000044.md): Longeron · cracked · Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/Stringer
  > DURING "C" CHECK, NR 3 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 323, CRACKED LONGERON AT NR 3 ENG LT CORE COWL UPPER AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.

Next page: https://openairdocs.org/model/douglas-dc-10-30f/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'DC1030F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-10-30f/reports

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