# Service difficulty reports: N526MD, cancelled Nov 1, 2012

A list on [N526MD, cancelled Nov 1, 2012](https://openairdocs.org/deregistered/N526MD-2012-11-01.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 2 · 57 reports

- [SDR 22AA201000067](https://openairdocs.org/sdr/22AA201000067.md): Receptacle · loose · Apr 5, 2010 · N526MD · Doug DC1030 · Cargo/Baggage Doors
  > PASSING FL 8000 AFT CARGO DOOR A & B LIGHT ILLUMINATED INTERMITTENT UNABLE TO PRESSURIZE, RETURN TO DEPARTURE. TROUBLE SHOOTING FOUND LOOSE CONNECTOR ON LATCH DOOR ACTUATOR IAW MM 52-33-02 AND OPS CHECKED GOOD IAW MM 52-33-00.
- [SDR 22AA201000037](https://openairdocs.org/sdr/22AA201000037.md): Clutch · out of adjust · Feb 15, 2010 · N526MD · Doug DC1030 · Power Lever
  > NR 1 THROTTLE BINDS CAUSING UNSAFE AUTO THROTTLE OPERATIONS, LUBE NR 1 ENGINE THROTTLE BUT STICKS ON AUTO THROTTLE, ENTERED ON DMI NR 23456, CAT "C" IAW MEL 22-7. ADJUSTED NR 1 AUTO THROTTLE CLUTCH IAW MM 22-31-05, TESTED IAW MM 22-31-05 FOUND NORMAL, THIS CL
- [SDR 22AA200900028](https://openairdocs.org/sdr/22AA200900028.md): Rub Strip · broken · Oct 9, 2009 · N526MD · Doug DC1030 · Trailing Edge Flaps
  > SERVICE CHECK FOUND RT INBD FLAP VANE RUBSTRIP BROKEN AND DAMAGE TO FLAP AND FLAP VANE. REMOVED AND REPLACED RT INBD FLAP VANE IAW AMM 27-50-03, OPS CK'D NORMAL.
- [SDR 22AA200900021](https://openairdocs.org/sdr/22AA200900021.md): Seat Track · corroded · Jul 2, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACKS AND LANDING SYS ARE CORRODED FROM STA 1884 TO 1941, LBL 20 TO RBL 10 (C-CHECK). REMOVED AND REPLACED SEAT TRACK SUPPORTS IAW SRM 51-31-01 NEW SEAT TRACK FABRICATED ON TRAVELER T9/796697. REPLACED HANDLING SYS AS REQUIRED IAW SRM 25-50-64. (K)
- [SDR 22AA200900017](https://openairdocs.org/sdr/22AA200900017.md): Seat Track · corroded · Jul 2, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION AND A LOADING SYS IS BROKEN AT STA 1990, RBL 50 APPROX (C-CHECK). REMOVED AND REPLACED SEAT TRACK SEC IAW SRM 51-31-01. NEW SEAT TRACK FABRICATED ON TRAVELER T9/796698 AND REPLACED BROKEN LOADING SYS IAW SRM 25-50-64. (K)
- [SDR 22AA200900014](https://openairdocs.org/sdr/22AA200900014.md): Seat Track · corroded · Jul 2, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > MCD SEAT TRACK AND LOADING SYSTEM HAS CORROSION FROM STA 1884 TO 2007, RBL 24 (C-CHECK). REMOVED AND REPLACED SEAT TRACK AND FLOOR BOARD SUPPORT IAW SRM 51-31-01, NEW FLOOR BOARD SUPPORT AND SEAT TRACK FABRICATED ON TRAVELER T9/796711 AND T9/796307 AND REPLAC
- [SDR 22AA2009000021](https://openairdocs.org/sdr/22AA2009000021.md): Cargo Track · corroded · Jul 2, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK - MCD SEAT TRACKS AND LOADING SYS ARE CORRODED FROM STA 1884 TO 1941, LBL 10 TO RBL 10. REMOVED AND REPLACED SEAT TRACK SUPPORTS IAW SRM 51-31-01. NEW SEAT TRACK FABRICATED ON TRAVELER T9/796697. REPLACED HANDLING SYS AS REQUIRED IAW ANCRA 25-50-64
- [SDR 22AA2009000017](https://openairdocs.org/sdr/22AA2009000017.md): Seat Track · corroded · Jul 2, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK - MCD SEAT TRACK HAS CORROSION AND LOADING SYS IS BROKEN AT STA 1990, RBL 50 APPROX. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 51-31-01. NEW SEAT TRACK FABRICATED ON TRAVELER T9/796698 AND REPLACED BROKEN LOADING SYS IAW ANCRA 25-50-64.
- [SDR 22AA2009000014](https://openairdocs.org/sdr/22AA2009000014.md): Seat Track · corroded · Jul 2, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK - MCD SEAT TRACK AND LOADING SYS HAVE CORROSION FROM STA 1884 TO 2007, LBL 24.0. REMOVED AND REPLACED SEAT TRACK AND FLOOR BOARD SUPPORT AND SEAT TRACK FABRICATED ON TRAVELER T9/796711 AND T9/796307 AND REPLACED 3 E/A HANDLING SYS FITTINGS IAW ANCRA
- [SDR 22AA200900019](https://openairdocs.org/sdr/22AA200900019.md): Seat Track · corroded · Jun 30, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STA 919 HAS (1 EA) AREA OF CORROSION. (C-CHECK) REPAIRED SEAT TRACK IAW SRM 53-70-00, FIG 1. (K)
- [SDR 22AA200900016](https://openairdocs.org/sdr/22AA200900016.md): Seat Track · corroded · Jun 30, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACT AT STA 1884 TO 2007, LBL 55 HAS HEAVY CORROSION. (C-CHECK) REMOVED AND INSTALLED FABED SEAT TRACK, REPAIRED IAW SRM 53-70-00, FIG 1. (K)
- [SDR 22AA200900015](https://openairdocs.org/sdr/22AA200900015.md): Seat Track · corroded · Jun 30, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > HCD SEAT TRACK HAS CORROSION UNDER AND AROUND LOADING STS AT STA 1990, RBL 24. (C-CHECK) REMOVED AND REPLACED (2 EA) FLOOR SUPPORTS IAW SRM 51-31-01, NEW SUPPORTS FABRICATED ON TRAVELER T9/796306 AND REINSTALLED HANDLING SYS IAW MM 25-50-64.
- [SDR 22AA200900013](https://openairdocs.org/sdr/22AA200900013.md): Seat Track · corroded · Jun 30, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CABIN FLOOR BOARD SUPPORT AT FS 1139, RBL 75 FASTENER HOLES CORRODED (C-CHECK). OPENED AREA IAW SRM 51-31-01, REMOVED AND REPLACED SEAT TRACK SECTION STA 1149-1129 IAW SRM 53-70-00, FIG 1 WITH PARTS FABRICATED ON MAE NR T9/796316, T9/796078, REPAIRED RB
- [SDR 22AA200900012](https://openairdocs.org/sdr/22AA200900012.md): Seat Track · corroded · Jun 30, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CABIN FLOORBOARD SUPPORT AT FS 1199 TO 1219, RBL 107 FASTENER HOLES CORRODED. (C-CHECK). CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00, FIG 5. REMOVED SEAT TRACK FROM STA 1189-1561 IAW SRM 51-31-01, SEAT TRACK FABRICATED ON TRAVELER NR T9/79569
- [SDR 22AA2009000019](https://openairdocs.org/sdr/22AA2009000019.md): Seat Track · corroded · Jun 30, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK - MCD SEAT TRACK AT STA 919 HAS 1 E/A AREA OF CORROSION. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1.
- [SDR 22AA2009000016](https://openairdocs.org/sdr/22AA2009000016.md): Seat Track · corroded · Jun 30, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK - MCD SEAT TRACK AT STA 1884 TO 2007 LBL 55 HAS HEAVY CORROSION. REMOVED AND INSTALLED FABRICATED SEAT TRACK. REPAIRED IAW SRM 53-70-00, FIG 1.
- [SDR 22AA2009000015](https://openairdocs.org/sdr/22AA2009000015.md): Seat Track · corroded · Jun 30, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK - MCD SEAT TRACK HAS CORROSION UNDER AND AROUND LOADING SYS AT STA 1990, RBL 24. REMOVED AND REPLACED 2 EA FLOOR SUPPORTS IAW SRM 51-31-01, NEW SUPPORTS FABRICATED ON TRAVELER T9/796306 AND REINSTALL HANDLING SYSTEM IAW ANCRA MM 25-50-64.
- [SDR 22AA2009000013](https://openairdocs.org/sdr/22AA2009000013.md): Floor Support · corroded · Jun 30, 2009 · N526MD · Doug DC1030 · Fuselage Miscellaneous Structure
  > "C" CHECK - UPPER CABIN FLOORBOARD SUPPORT AT FS 1139, RBL 75, FASTENERS HOLES CORRODED. OPENED AREA IAW SRM 51-31-01. REMOVED AND REPLACED SEAT TRACK SECTION STA 1159 - 1129 IAW SRM 53-70-00, FIG 1 WITH PARTS FABRICATED ON MAE NR T9/796316, T9/796078. REPA
- [SDR 22AA2009000012](https://openairdocs.org/sdr/22AA2009000012.md): Seat Track · corroded · Jun 30, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK - UPPER CABIN FLOORBOARD SUPPORT AT FS 1190 TO 1219, RBL 107 FASTENER HOLES CORRODED. CORROSION FOUND OUT OF LIMITS IAW SRM 53-70-00, FIG 5. REMOVED SEAT TRACK FROM STA 1189-1561 IAW SRM 51-31-01. SEAT TRACK FABRICATED ON TRAVELER NR T9/795690/ SP
- [SDR 22AA200900020](https://openairdocs.org/sdr/22AA200900020.md): Seat Track · corroded · Jun 28, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STA 1821-2007, RBL 75 IS CORRODED. (C-CHECK) REMOVED AND REPLACED SEAT TRACK AS REQUIRED, IAW SRM 53-70-00, FIG 1. (K)
- [SDR 22AA200900018](https://openairdocs.org/sdr/22AA200900018.md): Seat Track · corroded · Jun 28, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT STA 2000, LBL 107 IS CORRODED (C-CHECK). REMOVED AND REPLACED SEAT TRACK AS REQUIRED IAW SRM 53-70-00, FIG 1. (K)
- [SDR 22AA2009000020](https://openairdocs.org/sdr/22AA2009000020.md): Seat Track · corroded · Jun 28, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK - MCD SEAT TRACK AT STA 1821 - 2007, RBL 75 IS CORRODED. REMOVED AND REPLACED SEAT TRACK AS REQUIRED IAW SRM 53-70-00, FIG 1.
- [SDR 22AA2009000018](https://openairdocs.org/sdr/22AA2009000018.md): Seat Track · corroded · Jun 28, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK - MAIN DECK SEAT TRACK AT STA 2000, LBL 107 IS CORRODED. REMOVED AND REPLACED SEAT TRACK AS REQUIRED IAW SRM 53-70-00, FIG 1.
- [SDR 22AA200900011](https://openairdocs.org/sdr/22AA200900011.md): Seat Track · corroded · Jun 24, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CABIN FLOOR BOARD SUPPORT AT FS 1461 TO 1561, RBL 75 FASTENER HOLES CORRODED. (C-CHECK) REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REPLACED SEAT TRACK ON MAE TRAVELER (S) T9/796317 AND T9/795818. TREATED AND PRIMED IAW
- [SDR 22AA2009000011](https://openairdocs.org/sdr/22AA2009000011.md): Seat Track · corroded · Jun 24, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK - UPPER CABIN FLOORBOARD SUPPORT AT FS 1461 TO 1561 RBL 75; FASTENERS HOLES CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REPLACED SEAT TRACK ON MAE TRAVELER (S) T9/7963, T9/795818. TRATED AND PRIMED IAW SRM 51
- [SDR 22AA2009000010](https://openairdocs.org/sdr/22AA2009000010.md): Seat Track · corroded · Jun 24, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > "C" CHECK -LWR AFT CARGO COMPARTMENT SEAT TRACK AT RBL 20, STA 1872 IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT LWR AFT CARGO COMPARTMENT IAW SRM 51-31-01.
- [SDR 22AA200900009](https://openairdocs.org/sdr/22AA200900009.md): Cargo Track · corroded · Jun 24, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK - LWR AFT CARGO COMPARTMENT SEAT TRACK LBL 20, STA 1843 TO 1947 HAS SEVERAL AREAS CORRODED. REMOVED SEAT TRACK IAW SRM 51-31-01. ROUTED TO FABRICATE SEAT TRACK ON TRAVELER NR T9/794854. LOCATED AND DRILLED HOLES SEAT TRACK IAW SRM 51-31-01; TREATED
- [SDR 22AA200900010](https://openairdocs.org/sdr/22AA200900010.md): Seat Track · corroded · Jun 23, 2009 · N526MD · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > LWR AFT CARGO COMPT, SEAT TRACK AT RBL 20, STA 1872 IS CORRODED. (C-CHECK) REMOVED AND REPLACED SEAT TRACK AT LWR AFT CARGO COMPT RBL 20, STA 1841 TO 1967 IAW SRM 51-31-01. (K)
- [SDR 22AA20090601](https://openairdocs.org/sdr/22AA20090601.md): Slide · deflated · May 29, 2009 · N526MD · Doug DC1030F · Escape Slide
  > REFERENCE TO ROUTINE WORK CARD 180M250K; ACCOMPLISH DOOR ESCAPE SLIDE/RAFT OPS CHECK ON L-1 DOOR. OPS CHECK FAILED TO INFLATE SLIDE, DUE TO THE WIRE THAT SENDS THE ELECTRICAL SIGNAL TORE OFF AND BROKE AND THE MANUAL WAS DISCONNECTED. DEPLOYMENT OK. REMOVED AN
- [SDR 22AA20090504](https://openairdocs.org/sdr/22AA20090504.md): Skin · damaged · Mar 26, 2009 · N526MD · Doug DC1030 · Horizontal Stabilizer, Plate/Skin
  > RT SIDE OTBD AT HORIZONTAL STABILIZER TRAILING EDGE UPPER AND CENTER SECTION UPPER DAMAGE PERFORATION DUE TO NR 2 ENGINE DEBRIS. REFERENCE N/R NR 007. EWO'S ARW 55-001, ARW 55-002, ARW 55-003 WERE ACCOMPLISHED AT OTBD SECTION OF RT HORIZONTAL STABILIZER AND
- [SDR 22AA20090503](https://openairdocs.org/sdr/22AA20090503.md): Panel · punctured · Mar 26, 2009 · N526MD · Doug DC1030 · Horizontal Stabilizer, Plate/Skin
  > DURING INSPECTION WAS FOUND A PUNCTURE ON HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 344 - 461 RT DUE NR 2 ENGINE DEBRIS. HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 344 - 461 PUNCTURE RT REPAIR WAS ACCOMPLISHED IAW IAAC EO ARW-090414 BY TAMPA CARG
- [SDR 22AA20090502](https://openairdocs.org/sdr/22AA20090502.md): Panel · punctured · Mar 26, 2009 · N526MD · Doug DC1030 · Horizontal Stabilizer, Plate/Skin
  > DURING INSP, FOUND A PUNCTURE ON HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 247 - 344 RT DUE NR 2 ENGINE DEBRIS. HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 247 - 344 PINCTURE RT REPAIR WAS ACCOMPLISHED IAW IAAC EO ARW-090413.
- [SDR 22AA20090501](https://openairdocs.org/sdr/22AA20090501.md): Mount · damaged · Mar 26, 2009 · N526MD · Doug DC1030 · Engine Mount Section
  > FOUND AT AFT SECTION EXTENSIVE DAMAGE IN AFT PYLON AND NACELLE STRUCTURE, BY DEBRIS FROM ENGINE. REMOVED AND REPLACED AT AFT ENGINE MOUNT, TAIL PYLON TORQUE BOX IAW DC-10 DRAWING AVB7050 AND AVB 7326. REPLACED FASTENERS IAW DC-10 SRM 51-31-00 PAGE 1 TO 15 RE
- [SDR 22AA20090303](https://openairdocs.org/sdr/22AA20090303.md): Oil System · leaking · Mar 26, 2009 · N526MD · Doug DC1030F · Turbine Engine Oil System
  > LOG PAGE NR 126111. NR 2 ENGINE STARTED LOOSING OIL RAPIDLY. ACCOMPLISHED ENGINE FAILURE SHUTDOWN IN FLIGHT CHECK LIST. SHUTDOWN ENGINE AT 05:52Z AND REST OF FLIGHT UNEVENTFULL. REMOVED AND INSTALLED ENGINE IAW W/C 142R7101M. OPERATION TEST ON ENGINE RUN U
- [SDR 22AA20090302](https://openairdocs.org/sdr/22AA20090302.md): Structure · damaged · Mar 24, 2009 · N526MD · Doug DC1030F · Cargo/Baggage Doors
  > LOADER DAMAGED FAIRING AT THE FWD EDGE OF LWR CARGO DOOR (CTR). RED BORDER NR 025212 ACCOMPLISH TEMPORARY REPAIR OF CTR DOOR FAIRING DAMAGE IAW FLIGHT VRHICLES CONSULTING EO 53-03242009. REFERENCE F/V CONSULTING EO 53-03242009 PART 2 REPEAT INSP. PERFORMED TE
- [SDR 22AA20090301](https://openairdocs.org/sdr/22AA20090301.md): Seal · out of position · Mar 13, 2009 · N526MD · Doug DC1030 · Electrical/Electronic Compartment Doors
  > CABIN WOULD NOT HOLD PRESSURIZATION. BLEEDING FROM NR 1 & 3, PNEUMATIC SUPPLY OPEN. NR 1 AND NR 3 PACKS ON. TRIED ALL (4) MODES OF PRESSURIZATION & CABIN CONTINUED CLIMBING WITH ALL PACKS ON & OUTFLOW VALVE CLOSED. CABIN CONTINUED TO CLIMB & REACHED 12,000 CA
- [SDR 22AA20081004](https://openairdocs.org/sdr/22AA20081004.md): Engine · malfunctioned · Oct 25, 2008 · N526MD · Doug DC1030F · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF HEARD LOUD NOISE. TOWER ADVISED, FLAMES COMING FROM AIRCRAFT AND NR 1 ENGINE EGT WENT TO RED LINE. ENGINE SHUTDOWN ON ITS OWN. ENGINE CHANGE IN PROGRESS.
- [SDR 22AA20080906](https://openairdocs.org/sdr/22AA20080906.md): Inu · malfunctioned · Sep 28, 2008 · N526MD · Doug DC1030 · Inertial Guidance System
  > INERTIAL NAVIGATION SYSTEM (INS) NR 1 PRE-LAND TEST (PLT) FM FLOW OFF, LIGHT ON. ENTERED ON DMI 22099 IN ACCORDANCE WITH MEL 34-22, CATEGORY C. PLACARDS INSTALLED AS REQUIRED.
- [SDR ARWA20080905](https://openairdocs.org/sdr/ARWA20080905.md): Rheostat · failed · Sep 20, 2008 · N526MD · Doug DC1030 · Electrical Power System
  > CAPTAINS CHART HOLDER LIGHT IS CAUSING C/B E-8 TO POP. ELECT SMOKE ODOR AROUND CAPTAINS CHART HOLDER. FOUND CAPTAINS CHART HOLDER RHEOSTAT BAD. TRANSFERRED TO DMI NR 22073 AS PER MEL 33-1-0. CAT C. REPAIRED WIRE AT CAPTAINS CHART HOLDER IN ACCORDANCE WITH
- [SDR ARWA20080504](https://openairdocs.org/sdr/ARWA20080504.md): Wire · broken · May 17, 2008 · N526MD · Doug DC1030 · Pneumatic System Wiring
  > NR 3 ENGINE PNEUMATIC PRESSURE GAUGE INDICATING 40 PSI W/PNEUMATIC SUPPLY SWITCH IN THE OFF POSITION. REPAIRED BROKEN WIRE AT ELECTRICAL CONNECTOR ON NR 3 ENGINE PNEUMATIC PRESSURE REGULATOR VALVE IN ACCORDANCE WITH DC10 M/M 36-12-01 AND OPERATIONAL CHECK FOU
- [SDR ARWA20080302](https://openairdocs.org/sdr/ARWA20080302.md): Altimeter · intermittent · Mar 2, 2008 · N526MD · Doug DC1030 · Altimeter, Barometric/Encoder
  > FIRST OFFICER'S ALTIMETER INTERMITTENTLY STICKS IN FLIGHT; OCCASIONALLY HAS OFF FLAG IN VIEW. REMOVED AND REPLACED FIRST OFFICER'S ALTIMETER IN ACCORDANCE WITH M/M 34-12-01; PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH M/M 34-12-00 AND 34-16-00 FOUND NORMAL
- [SDR ARWA20080102](https://openairdocs.org/sdr/ARWA20080102.md): Indicator · malfunctioned · Jan 24, 2008 · N526MD · Doug DC1030 · Airspeed/Mach Indicator
  > FIRST OFFICER'S AIRSPEED INDICATOR DISPLAYS FAIL-FLAG IN VIEW; REVISED AND PERFORMED EXPANDED CHECKLIST UNABLE TO RESTORE. REMOVED AND REPLACED FIRST OFFICER'S MACH AIRSPEED INDICATOR IN ACCORDANCE WITH M/M 34-13-01. OPERATIONAL CHECK TEST FOUND NORMAL IN AC
- [SDR ARWA20071207](https://openairdocs.org/sdr/ARWA20071207.md): Computer · malfunctioned · Dec 6, 2007 · N526MD · Doug DC1030 · Air Data Computer
  > FIRST OFFICER'S (FO) ALTIMETER ERRATIC; READS + 500 FT AT TIMES. REMOVED AND REPLACE NR 2 DIGITAL AIR DATA COMPUTER IN ACCORDANCE WITH M/M 34-16-01. PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH M/M 34-16-00, FOUND NORMAL. ALSO PERFORMED PITOT STATIC LEAK C
- [SDR ARWA20070605](https://openairdocs.org/sdr/ARWA20070605.md): Engine · low pressure · Jun 10, 2007 · N526MD · Doug DC1030 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF ROLL, NR 3 ENGINE AT FIREWALL THRUST 98 PERCENT N1, N2, EGT AND FUEL FLOW LOW; ABORTED TAKEOFF. PERFORMED TROUBLESHOOTING IN ACCORDANCE WITH M/M 72-00-00; FLUSHED COMPRESSOR DISCHARGE SENSE LINE AND PERFORMED MPA RUN AT BLAST FENCE, ALL PARAMET
- [SDR ARWA20050910](https://openairdocs.org/sdr/ARWA20050910.md): Engine · malfunctioned · Sep 18, 2005 · N526MD · Doug DC1030 · Engine (Turbine/Turboprop)
  > ON TAKEOFF, NR 1 ENGINE ADVANCED TO 40 PERCENT N1 AND WOULD NOT GO BEYOND, ALL OTHER PARAMETERS NORMAL. ENTERED ON DMI NR19537 AS PER MEL 77-11-1 CAT "B" REFER TO DDG 77-1 C/W. PERFORMED NR 1 ENGINE RUN-UP IN ACCORDANCE WITH M/M 71-00-00. FOUND N1 INDICATIO
- [SDR ARWA20050802](https://openairdocs.org/sdr/ARWA20050802.md): Engine · fire · Aug 12, 2005 · N526MD · Doug DC1030 · Fire Detection
  > ON CLIMBOUT, NR 1 ENGINE FIRE LIGHT AND BELL. ENGINE FIRE SEVERE DAMAGE CHECK COMPLIED WITH. REMOVED AND REPLACED NR 1 ENGINE LOWER FIRE DETECTOR TUBE ASSEMBLY AND "A" SENSING FIRE LOOP/GROMMETS IN ACCORDANCE WITH M/M 26-11-01 AND INSPECTED FOR ANY LEAKS PNE
- [SDR ARWA20050703](https://openairdocs.org/sdr/ARWA20050703.md): Line · leaking · Jul 24, 2005 · N526MD · Doug DC1030 · Hydraulic System, Main
  > FOUND HYDRAULIC LINE LEAKING; LOCATED ON TOP OF RIGHT LANDING GEAR WHEEL WELL. REPAIRED HYDRAULIC LINE IN ACCORDANCE WITH DC-10 M/M 20-10-01. NO LEAKS FOUND IN ACCORDANCE WITH DC-10 M/M 29-00-00
- [SDR ARWA20050402](https://openairdocs.org/sdr/ARWA20050402.md): Line · broken · Apr 5, 2005 · N526MD · Doug DC1030 · Hydraulic System, Main
  > DURING TAXI, TOTAL LOSS OF HYDRAULIC SYSTEM NR 3 FLUID. T/S FOUND BROKEN LINE FROM NR 3 SYSTEM IN CENTER WHEEL WELL. REPAIRED LINE IN ACCORDANCE WITH DC-10 M/M 20-10-01. SERVICED NR 3 HYDRAULIC SYSTEM IN ACCORDANCE WITH M/M 12-13-02. NO LEAKS NOTED.
- [SDR ARWA20041202](https://openairdocs.org/sdr/ARWA20041202.md): Duct · defective · Dec 11, 2004 · N526MD · Doug DC1030 · Pneumatic Distribution System
  > AFTER TAKEOFF AND ENGINE IN CLIMB POWER TURNED NR 2 PNEUMATIC SUPPLY SWITCH TO AUTO NR MANIFOLD LIGHT CAME ON. REMOVED DEFECTIVE PNEUMATIC DUCT (LT) BETWEEN FUSELAGE STATION 1239 AND STA 1361 IN ACCORDANCE WITH DC-10-30 MM 36-14-02. INSTALLED NEW PNEUMATIC D
- [SDR WRLA200403](https://openairdocs.org/sdr/WRLA200403.md): Slide · failed · Jan 6, 2004 · N526MD · Doug DC1030 · Escape Slide
  > DURING ROUTINE DEPLOYMENT CHECK OF L1 DOOR SLIDERAFT PER WORLD TASK CARD 101C-022, TIMCO W/O 107021, THE SLIDE RAFT DEPLOYED INWARD AS THE DOOR WAS APPROXIMATELY HALF OPEN. THE SLIDE DID NOT FALL OUT OF THE DOOR OPENING AS DURING NORMAL DEPLOYMENT. REMOVED A

Next page: https://openairdocs.org/deregistered/N526MD-2012-11-01/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 = 'N526MD' AND deregistration_id = 'N526MD-2012-11-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N526MD-2012-11-01/reports

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