# Service difficulty reports: N68056, cancelled Sep 30, 2009 A list on [N68056, cancelled Sep 30, 2009](https://openairdocs.org/deregistered/N68056-2009-09-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 150 reports - [SDR 07FDEA02519](https://openairdocs.org/sdr/07FDEA02519.md): Stiffener · cracked · Jul 18, 2007 · N68056 · Doug MD1010F · Nacelle/Pylon, Main Frame > NR 1 PYLON HAS 6" CRACK VERTICAL STRUCTURE SUPPORT ON OUTBOARD BULKHEAD. VIEWED THROUGH ACCESS PANEL AUB7025-3 APPROXIMATE 4 FEET FWD PYLON STATION YN=358. [08-24-07] REMOVED AND REPLACED STIFFENER BRACKET AS REQUIRED, REF. DAC DRAWING AUB 7087. 09-04-07 - [SDR 06FDEA1550](https://openairdocs.org/sdr/06FDEA1550.md): Panel · cracked · Apr 20, 2006 · N68056 · Doug MD1010F · Horizontal Stabilizer, Plate/Skin > DURING NDT INSPECTION, FOUND 4 PANEL CRACKED, HORIZ STAB ZONE. REPLACED PANELS ON CENTER BOX STABILIZER AND LT STABILIZER IAW EA #8-5510-93812. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164297/N01297 AND IAW SB 55-16 FIG 5. - [SDR 06FDEA1022](https://openairdocs.org/sdr/06FDEA1022.md): Door Frame · damaged · Mar 13, 2006 · N68056 · Doug MD1010F · Fuselage Main, Structure > MAIN CABIN FOUND NR 1EA CRACK ON WEB JAMB DOOR NR 3 AFT AT STA 1305 LONG 15 RT SIDE. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1, FAB PART IAW DETAIL PART TRAVELER F163495/N00495 AND IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1. - [SDR 06FDEA1020](https://openairdocs.org/sdr/06FDEA1020.md): Skin · cracked · Mar 13, 2006 · N68056 · Doug MD1010F · Wing, Plate/Skin > LEFT WING UPPER SURFACE T/E FOUND 1EA CRACK ON HONEYCOMB PANEL AT XORS 299. REPAIRED PANEL IAW SRM 57-00-01 FIG 1 SHT 1 VOL 1 AND SRM 51-70-00 PARA 16 VOL 2, FABRICATED PART IAW DETAIL PART TRAVELER F163459/N00459 AND IAW SRM 57-00-01 AND 51-70-00 VOL 1-2. - [SDR 06FDEA0983](https://openairdocs.org/sdr/06FDEA0983.md): Repair · damaged · Mar 8, 2006 · N68056 · Doug MD1010F · Fuselage Main, Plate/Skin > FOUND EXTERNAL DOUBLER REPAIR AT RIGHT AIR CONDITIONING COMPT DOOR AT APPROX STA 515. INSTALLED REPAIR FILLERS, REPAIR STRAP, AND REPAIR ANGLE, AND REPAIR DOUBLER IAW SRM 52-10-00 FIG 2 AND SRM 53-00-01 FIG 4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER - [SDR 06FDEA0944](https://openairdocs.org/sdr/06FDEA0944.md): Repair · unknown · Mar 6, 2006 · N68056 · Doug DC1010 · Trailing Edge Flaps > LEFT WING O/B FLAP T/E AREA FOUND AN EXTERNAL DOUBLER REPAIR BETWEEN WING STA XOF 563 AND XOF 575. REMOVED T/E IAW SRM 51-35-01 PAGE 1-13 VOL 2 AND DWG ARC1653, CUT AND REMOVED CRACKED SECTION AND REPAIRED IAW SRM 57-00-01 FIG 10 SHT 2 VOL 1 AND SRM 51-00-01 - [SDR 06FDEA0943](https://openairdocs.org/sdr/06FDEA0943.md): Skin · cracked · Mar 6, 2006 · N68056 · Doug DC1010 · Fuselage Main, Plate/Skin > LWR FUSELAGE EXT STRUCTURE FOUND 1EA CRACK 0.25 INCH LONG ON SKIN AT STA 595 BETWEEN LONG NR 48 LEFT AND LONG NR 47 LEFT NEAR CORNER OF EXHAUST. REMOVED RAM AIR EXHAUST IAW MM 21-55-02-4, PERFORMED PENETRANT INSP IAW MM 20-20-00. INSTALLED DOUBLERS IAW SRM 5 - [SDR 06FDEA0942](https://openairdocs.org/sdr/06FDEA0942.md): Skin · cracked · Mar 6, 2006 · N68056 · Doug DC1010 · Trailing Edge Flaps > LEFT WING O/B FLAP UPPER SKIN SURFACE STA XOF 575 FOUND CRACK 2 INCHES LONG BETWEEN INTERCOSTAL PLANE NR 1 AND NR 2. REMOVED AND REINSTALLED SECTION T/E IAW SRM 51-31-01 PAGE 36/41 VOL 2 AND REPAIRED SKIN DAMAGE IAW SRM 57-10-00 FIG 65 VOL 1. FABRICATED PART - [SDR 06FDEA0895](https://openairdocs.org/sdr/06FDEA0895.md): Bolt · misinstalled · Mar 2, 2006 · N68056 · Doug DC1010 · Aircraft Structures > DISCREPANCY FUSELAGE STA 275 FWD PRESSURE BULKHEAD DURING VISUAL INSP IAW EA NR 8-5310-79443B P2 FOUND INSTALLED BOLT INSTEAD OF LOCK FASTENERS. REMOVED MECH ASSY STEERING IAW MM 20-50-02-2 ACCOMPLISHED EA NR8-5310-79443B. REINSTALLED MECH AND PERFORMED TES - [SDR 06FDEA0903](https://openairdocs.org/sdr/06FDEA0903.md): Web · cracked · Mar 2, 2006 · N68056 · Doug DC1010 · Fuselage Miscellaneous Structure > UPPER CARGO AREA STA 1256 L15 LEFT SIDE FOUND WEB CRACK ON THE RADIUS ON L3 JAMB DOOR.5 INCH LONG. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163479/N00479 AND IAW SRM 53-50-00 FIG 19 VOL 1. - [SDR 06FDEA0904](https://openairdocs.org/sdr/06FDEA0904.md): Structure · cracked · Mar 2, 2006 · N68056 · Doug DC1010 · Fuselage Main, Structure > CTR CARGO COMPT CRACK 5 INCHES LONG ON FWD DOOR JAMB. REMOVED CRACKED SECTION IAW SRM 51-35-01 PG 1/13 VOL 2 AND SRM 51-33-01 PG 34/47 VOL 2. FABRICATED AND INSTALLED NEW PAN SECTION AND OLD SPLICE IAW SRM 52-00-01 FIG 7 VOL 1 IAW SRM 51-35-01 PG 1-13 VOL 2 - [SDR 06FDEA0905](https://openairdocs.org/sdr/06FDEA0905.md): Bulkhead · cracked · Mar 2, 2006 · N68056 · Doug DC1010 · Fuselage Main, Bulkhead > CLG WHEEL WELL SPACE FOUND 4EA CRACKS FROM.5" INCH TO 2 INCHES LONG ON UPPER SIDE LEFT VERTICAL BULKHEAD FROM STA 1491 TO 1501 LEFT SIDE X 31. INSTALLED CABLE, PULLEY, ACCUMULATOR AND PIPES IAW MM 27-51-07-2 AND MM 27-51-09-2 AND MM 20-10-01-2 AND MM 29-12 - [SDR 06FDEA0906](https://openairdocs.org/sdr/06FDEA0906.md): Skin · cracked · Mar 2, 2006 · N68056 · Doug DC1010 · Trailing Edge Flaps > RIGHT WING O/B FLAP T/E FROM STA XOF 458 TO XOF 467 FOUND 1EA CRACK 2 INCHES LONG ON UPPER SURFACE SKIN, 1EA CRACK ON INT CHANNEL REF SRM 57-52-01 PG 52, MANY RIVETS LOOSE ON UPPER AND LOWER SURFACE. CUT AND REMOVED T/E CHANNEL AND REPAIRED IAW SRM 57-20-00 F - [SDR 06FDEA0820](https://openairdocs.org/sdr/06FDEA0820.md): Intercostal · cracked · Feb 24, 2006 · N68056 · Doug DC1010 · Passenger/Crew Doors > ON DOOR NR 3 RT FOUND 1EA CRACK 0.50 INCH LONG ON INTERCOSTAL SPLICE AT STA 1256 BETWEEN DOOR BEAM NR 5 AND NR 6 (REMOVED PART). BLENDED OUT DAMAGE AREA IAW SRM 52-00-01 FIG 1A SHT 1 VOL 1 AND REPAIRED INSTALLED DOUBLER IAW SRM 52-00-01 FIG 7 SHT 1 VOL 1 STEP - [SDR 06FDEA0819](https://openairdocs.org/sdr/06FDEA0819.md): Intercostal · cracked · Feb 24, 2006 · N68056 · Doug DC1010 · Passenger/Crew Doors > ON DOOR NR 3 RT FOUND NR 1EA CRACK 0.50 INCH LONG ON INTERCOSTAL SPLICE AT STA 1305 BETWEEN DOOR BEAM NR 5 AND NR 6 (REMOVED PART). BLENDED OUT DAMAGE PART IAW SRM 52-00-01 FIG 1A SHT 1 VOL 1 AND INSTALLED REPAIRED DOUBLER IAW SRM 52-00-01 FIG 7 SHT 1 VOL 1 - [SDR 06FDEA0683](https://openairdocs.org/sdr/06FDEA0683.md): Skin · dented · Feb 14, 2006 · N68056 · Doug DC1010 · Elevator, Plate/Skin > RT ELEVATORS FOUND DEEP DENT ON SKIN AT STA XE 136 UPPER SURFACE. TRIMMED OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163412/N00412 AND IAW SRM 55-10-00 FIG 8 VOL 1. - [SDR 06FDEA0682](https://openairdocs.org/sdr/06FDEA0682.md): Bulkhead · cracked · Feb 14, 2006 · N68056 · Doug DC1010 · Fuselage Main, Bulkhead > AFT BODY BLKHD EXT STRUCTURE FOUND 1 CRACK 0.50" LONG ON HORIZONTAL LONGERON AT STA 2163.685 X37 LT SIDE. REPAIRED CRACKED STIFFENER IAW SRM 53-40-00 FIG 7 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163376/N00376 AND IAW SRM 53-40-00 FIG 7 VOL 1. - [SDR 06FDEA0627](https://openairdocs.org/sdr/06FDEA0627.md): Channel · broken · Feb 9, 2006 · N68056 · Doug DC1010 · Wing Miscellaneous Structure > LT WING L/E AT PYLON INTERSECTION ZONE 517 STA XDLE 315 FOUND CHANNEL BROKEN 1"1/2 LONG AND NUTPLATE MISSING ON THE AFT SECTION REF SRM 57-21-01 PAGE 18 ITEM 2. REMOVED SKIN IAW SRM 51-31-01 PAG 36/41 VOL 2 AND INTERCOSTAL IAW SRM 51-35-01 PAGE 1/13 VOL 2. T - [SDR 06FDEA0626](https://openairdocs.org/sdr/06FDEA0626.md): Rib · cracked · Feb 9, 2006 · N68056 · Doug DC1010 · Wing, Rib/Bulkhead > FUEL TANK NR 1 STA XORS 372 BELOW STR 12 UPPER RIB CHORD FOUND CRACKED. REPAIRED CRACK IAW SRM 57-20-00 FIG 38 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER NRC F163636/N00636 IAW SRM 57-20-00 FIG 38 VOL 1. - [SDR 06FDEA0545](https://openairdocs.org/sdr/06FDEA0545.md): Skin · cracked · Feb 6, 2006 · N68056 · Doug DC1010 · Trailing Edge Flaps > RT WING OUTBOARD FLAP CRACK 1,5" LONG AND NR 20 FASTENERS U/S ON UPPER SKIN AT STA XOF 542. TRIMMED OUT CRACK AND REPAIRED IAW SRM 57-10-00 FIG 85 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163355/N00355 AND IAW SRM 57-10-00 FIG 85 VOL 1. - [SDR 06FDEA0544](https://openairdocs.org/sdr/06FDEA0544.md): Hinge · cracked · Feb 6, 2006 · N68056 · Doug DC1010 · Wing Main, Frame Structure > FOUND LT WING L/E XOS 792 FOUND ACCESS PANEL TEE/HINGE CRACK 1" LONG AND EXT SKIN LOWER SECTION CRACK 2" LONG. REPAIRED L/E SKIN IAW SRM 57-10-00 FIG 68 VOL 1 AND SRM 57-10-00 FIG 49 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F163378/N00378 AND IAW SR - [SDR 06FDEA0543](https://openairdocs.org/sdr/06FDEA0543.md): Skin · damaged · Feb 6, 2006 · N68056 · Doug DC1010 · Trailing Edge Flaps > RIGHT WING LOWER SURFACE OUTBOARD FLAP FOUND REPAIR AT TRAILING EDGE SECTION AT APPROX STA XOS 470. SCRAPED DOUBLER OF EXISTING EA REMOVED DAMAGED SECTION OF SKIN AND REPAIRED IAW SRM 57-10-00 FIG 7 SHT 3 VOL 1 FABRICATED PART IAW DETAIL PART TRAVELER F163850 - [SDR 06FDEA0542](https://openairdocs.org/sdr/06FDEA0542.md): Repair · unknown · Feb 6, 2006 · N68056 · Doug DC1010 · Fuselage Main, Plate/Skin > RIGHT SIDE BELOW AND FWD OG R-2 DOOR FOUND EXT DOUBLER REPAIR BETWEEN STA 735 AND 755 AND LONGERONS 29 TO 31. REMOVED EXISTING REPAIR AND INSTALLED REPAIR IAW SRM 53-20-00 FIG 11 AND SRM 53-20-00 FIG 6 VOL 1. - [SDR 06FDEA0541](https://openairdocs.org/sdr/06FDEA0541.md): Skin · cracked · Feb 6, 2006 · N68056 · Doug DC1010 · Wing, Plate/Skin > FOUND LT WING L/E XOS 613 FOUND CRACK 1" LONG ON THE REFUEL DOOR VANE EXTERNAL SKIN. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 68 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163380/N00380. - [SDR 06FDEA0540](https://openairdocs.org/sdr/06FDEA0540.md): Skin · cracked · Feb 6, 2006 · N68056 · Doug DC1010 · Wing, Plate/Skin > RT WING L/E FOUND CRACK 2" LONG ON EXT SKIN AT STA XORS 480. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 2-3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163612/N00612 AND IAW SRM 57-10-00 FIG 68 SHT 2 VOL 1. - [SDR 06FDEA0247](https://openairdocs.org/sdr/06FDEA0247.md): Tank · cracked · Jan 18, 2006 · N68056 · Doug DC1010 · Fuselage Miscellaneous Structure > AFT FUSELAGE WASTE TANK COMPT FOUND 1EA CRACK ON LONG 43, 3 INCHES LONG BETWEEN STA 1986 AND 1997 LT. REMOVED FRAME SPLICE AND ANGLES AND REINSTALLED PARTS IAW SRM 51-35-01 PAGE 1-13, DWG AJC7363, DWG NJC6074 AND SRM 51-33-01 PAGE 34-47 VOL 2. CUT LONGERONS - [SDR 06FDEA0246](https://openairdocs.org/sdr/06FDEA0246.md): Skin · cracked · Jan 18, 2006 · N68056 · Doug DC1010 · Wing, Plate/Skin > LEFT WING EXTERNAL SKIN OF L/E SLAT TRACK NR 10 XOS 660 FOUND CRACK.5 INCH LONG ON THE SLAT TRACK HOLE ANGLE. INSTALLED EXTERNAL DOUBLER IAW SRM 57-10-00 FIG 68 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER F163379/N00379 AND IAW SRM 57-10-00 FIG 68 VOL 1. - [SDR 06FDEA0154](https://openairdocs.org/sdr/06FDEA0154.md): Door Frame · cracked · Jan 12, 2006 · N68056 · Doug DC1010 · Fuselage Main, Structure > MAIN CABIN FOUND 2 EA CRACKS 1 INCH LONG AND.50 INCH LONG ON WEB JAMB DOOR 3 FWD AT STA 1256 LONG 27 RT. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 1 VOL. FABRICATED PART IAW DETAIL PART TRAVELER F163498/N00498 AND IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. - [SDR 05FDEA04282](https://openairdocs.org/sdr/05FDEA04282.md): Bulkhead · cracked · Dec 13, 2005 · N68056 · Doug DC1010 · Fuselage Main, Bulkhead > FOUND LT AIR CONDITIONING COMPT FOUND 1 CRACK 4" LONG ON SKIN OF BULKHEAD BETWEEN STA 584 AND STA 580 Z-46 BY 24. TRIMMED OUT CRACK AND INSTALLED FILLER AND 2 REPAIRED DOUBLERS IAW SRM 53-30-00 FIG 6 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F1 - [SDR 05FDEA04151](https://openairdocs.org/sdr/05FDEA04151.md): Frame · cracked · Dec 6, 2005 · N68056 · Doug DC1010 · Fuselage Main, Frame > CAC LOWER LOBE BILGE FOUND 1EA CRACK, 3 INCHES LONG ON LT FRAME AT STA 1159 CLOSE TO PRESSURE PANEL FWD CENTER WING. REMOVED ATTACH ANGLE IAW SRM 51-33-01 PAR 6-10 VOL 2 REPAIRED FRAME IAW SRM 53-30- 00 FIG 7 VOL 1 REINSTALLED ATTACH ANGLE IAW SRM 51-33-01 P - [SDR 05FDEA04150](https://openairdocs.org/sdr/05FDEA04150.md): Doubler · none · Dec 6, 2005 · N68056 · Doug DC1010 · Aircraft Structures > DISCREPANCY FOUND EXTERNAL DOUBLER BETWEEN STA 735 AND 755 AND LONGERONS 34 AND 35 LT SIDE, WHERE POTABLE WATER SERVICE PANEL USED TO BE LOCATED. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 6 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8- - [SDR 05FDEA03973](https://openairdocs.org/sdr/05FDEA03973.md): Hinge · cracked · Nov 28, 2005 · N68056 · Doug DC1010 · Wing Main, Frame Structure > LT WING LEADING EDGE AT STA XOS 906 FOUND ACCESS PANEL TEE/HINGE CRACK.5 INCH LONG. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F163377/N00377 AND IAW SRM 57-10-00 FIG 49 VOL 1. - [SDR 05FDEA03972](https://openairdocs.org/sdr/05FDEA03972.md): Flange · cracked · Nov 28, 2005 · N68056 · Doug DC1010 · Fuselage Main, Bulkhead > CLG WHEEL WELL/SPACE: 1EA CRACK 1 INCH LONG ON DOUBLER FLANGE UPPER SIDE LT VERTICAL BULKHEAD FROM STA 1421 TO 1431 LT SIDE X 31. REMOVED DOUBLER IAW SRM 51-35-01 PG 1/13 VOL 2. CLEANED UP CRACK REPAIRED IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1 WITH FILLER AND REI - [SDR 05FDEA03955](https://openairdocs.org/sdr/05FDEA03955.md): Repair · proper · Nov 24, 2005 · N68056 · Doug DC1010F · Fuselage Main, Plate/Skin > FWD OF FWD CARGO DOOR STA 859 BETWEEN STRINGERS 36 AND 37 ON THE RT SIDE THERE IS AN INTERNAL DOUBLER REPAIR. PERFORMED A INSPECTION OF REPAIR IAW EA#8-5330-93229 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO#8-5100-7-5001-P1 E3. - [SDR 05FDEA03954](https://openairdocs.org/sdr/05FDEA03954.md): Repair · unknown · Nov 24, 2005 · N68056 · Doug DC1010 · Fuselage Main, Frame > FWD AVIONICS COMPT AT STA 475 FOUND FRAME REPAIR AT X 60. NO ACTION TAKEN FRAME WILL BE REMOVED WITH NRC N00579. - [SDR 05FDEA03953](https://openairdocs.org/sdr/05FDEA03953.md): Door Frame · cracked · Nov 24, 2005 · N68056 · Doug DC1010 · Fuselage Main, Structure > MAIN CABIN FOUND 2 CRACKS 1" LONG ALL ON WEB JAMB DOOR NR 3 AFT AT STA 1305 LONG 27 RT SIDE. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163497/N00497 AND IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1. - [SDR 05FDEA03952](https://openairdocs.org/sdr/05FDEA03952.md): Bulkhead · cracked · Nov 24, 2005 · N68056 · Doug DC1010 · Fuselage Main, Bulkhead > RT AIR CONDITIONING COMPT FOUND 1 CRACK 2.50" LONG ON BULKHEAD BETWEEN STA 575 AND STA 569 Z-60 X-24. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164142/N001142 AND IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. - [SDR 05FDEA03836](https://openairdocs.org/sdr/05FDEA03836.md): Angle · cracked · Nov 16, 2005 · N68056 · Doug DC1010 · Fuselage Miscellaneous Structure > RIGHT AIR CONDITIONING COMPT FOUND 1 CRACK 1" LONG ON TEE ANGLE AT STA 535 Z-39 X-102. REPAIRED CRACK IAW SRM 53-00-01 FIG 9 SHT 7 VOL 1. - [SDR 05FDEA03834](https://openairdocs.org/sdr/05FDEA03834.md): Bulkhead · cracked · Nov 16, 2005 · N68056 · Doug DC1010 · Fuselage Main, Bulkhead > RT AIR CONDITIONING COMPT FOUND 1 CRACK 2 INCHES LONG ON BULKHEAD BETWEEN STA 482 AND STA 489 Z-60 X-24. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1, FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164141/N01141 AND IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. - [SDR 05FDEA03823](https://openairdocs.org/sdr/05FDEA03823.md): Repair · proper · Nov 15, 2005 · N68056 · Doug DC1010 · Landing Gear Doors > JUST ABOVE FWD NOSE LANDING GEAR DOOR BETWEEN STA 490 AND 555 LT SIDE, FOUND FLUSH DOUBLER OF APROX 62 X 25 INCH. PERFORMED A GVI OF REPAIRS IAW CONTINENTAL AIRLINES EC/RA 253C038, 253C039, 253C040, 253C042, 253C044 AND FOUND IN COMPLIANCE WITH CRITERIA REQUE - [SDR 05FDEA03822](https://openairdocs.org/sdr/05FDEA03822.md): Repair · proper · Nov 15, 2005 · N68056 · Doug DC1010 · Fuselage Main, Structure > FOUND FLUSH DOUBLER REPAIR RT SIDE BETWEEN STA 490 AND 535 JUST ABOVE OF FWD NOSE LANDING GEAR ON AN AREA OF ABOUT 43'' BY 21''. PERFORMED A GVI OF REPAIRS IAW CONTINENTAL AIRLINES EC/RA NO 253C042 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO#8-5100-7 - [SDR 05FDEA03821](https://openairdocs.org/sdr/05FDEA03821.md): Repair · proper · Nov 15, 2005 · N68056 · Doug DC1010 · Fuselage Main, Structure > FOUND EXTENSIVE DOUBLER REPAIR AROUND L-1 DOOR BETWEEN STA 401 AND 470.25 BOTTOM FWD AND AFT CORNERS ON FUSELAGE SKIN. PERFORMED A GVI OF EXISTING DOUBLER IAW FEDEX EA NR 8-5300-26224 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001. - [SDR 05FDEA03796](https://openairdocs.org/sdr/05FDEA03796.md): Door Frame · cracked · Nov 14, 2005 · N68056 · Doug DC1010F · Fuselage Main, Structure > MAIN CABIN, FOUND 1 CRACK.25" LONG ON WEB JAMB DOOR NR 3 FWD AT STA 1256 LONG 15 RT. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163496/N00496 AND IAW SRM 53-50-00 FIG 19 VOL 1. - [SDR 05FDEA03798](https://openairdocs.org/sdr/05FDEA03798.md): Repair · undamaged · Nov 14, 2005 · N68056 · Doug DC1010F · Fuselage Main, Structure > BARON REPAIR, DOUBLER INSTALLED AT APPROX STA 505 RT SIDE BETWEEN LONG 39 AND 40. PERFORMED A GVI OF BARON DOUBLER IAW FEDEX EA NR 8-5320-38573B AND FEDEX EA NR 8-5320-35995A AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001. - [SDR 05FDEA03799](https://openairdocs.org/sdr/05FDEA03799.md): Repair · proper · Nov 14, 2005 · N68056 · Doug DC1010 · Fuselage Main, Bulkhead > FOUND FWD PRESSURE BULKHEAD STA 275 LT HAND SIDE FOUND REPAIR DOUBLER BETWEEN X 13, X28 AND Z-14, Z-27.7 BEAMS. PERFORMED A GVI OF DOUBLER IAW CONTINENTAL AIRLINES EC/RA #253C037 AND FEDEX EA#8-5310-79443B AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# - [SDR 05FDEA03710](https://openairdocs.org/sdr/05FDEA03710.md): Door Frame · unknown · Nov 8, 2005 · N68056 · Doug DC1010 · Fuselage Main, Structure > FOUND MAIN CABIN L-3 DOOR FWD DOOR JAMB STA 1259 FOUND DOUBLER REPAIR BETWEEN STRINGER 24 AND 27. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-50-00 FIG 19. - [SDR 05FDEA03709](https://openairdocs.org/sdr/05FDEA03709.md): Repair · undamaged · Nov 8, 2005 · N68056 · Doug DC1010 · Fuselage Main, Plate/Skin > FOUND EXTERNAL TRIPLE DOUBLER REPAIR AT STA 1139 BETWEEN LONGERON 47 AND 48 RT SIDE. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-20-00 FIG 6. - [SDR 05FDEA03708](https://openairdocs.org/sdr/05FDEA03708.md): Skin · unknown · Nov 8, 2005 · N68056 · Doug DC1010 · Fuselage Main, Plate/Skin > FOUND MAIN CABIN BETWEEN FUSELAGE STA 1601 AND 1621, STRINGERS 8 AND 9 RT SIDE FOUND A FLUSH REPAIR. PERFORMED A GVI OF EXISTING REPAIR IAW SRM 53-20-00 FIG 13 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001. - [SDR 05FDEA03707](https://openairdocs.org/sdr/05FDEA03707.md): Repair · undamaged · Nov 8, 2005 · N68056 · Doug DC1010 · Air Conditioning Doors > AFT AIR CONDITIONING ACCESS DOOR, AFT TOP CORNER FOUND AN EXTERNAL TRIPLE DOUBLER REPAIR AT STA 595 LT SIDE. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND IN COMPLIANCE WITH SRM 53-50-00 PAG 19. - [SDR 05FDEA03706](https://openairdocs.org/sdr/05FDEA03706.md): Repair · undamaged · Nov 8, 2005 · N68056 · Doug DC1010 · Fuselage Main, Structure > AFT FUSELAGE ABOVE HORIZONTAL STABILIZER LT SIDE STA Y2131 FOUND AN EXTERNAL DOUBLER REPAIR. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-00-01 FIG 4. Next page: https://openairdocs.org/deregistered/N68056-2009-09-30/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 n_number = 'N68056' AND deregistration_id = 'N68056-2009-09-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N68056-2009-09-30/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.