# Service difficulty reports: Douglas DC-8-72

A list on [Douglas DC-8-72](https://openairdocs.org/model/douglas-dc-8-72.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 201 reports

- [SDR 2021F00362](https://openairdocs.org/sdr/2021F00362.md): Duct · cracked · Nov 22, 2021 · N782SP · Doug DC872 · Pneumatic Distribution System
  > FORWARD CARGO COMPARTMENT PNEUMATIC DUCT FOUND WITH 6" CRACK. REF NRC# B000386.
- [SDR 2022F00019](https://openairdocs.org/sdr/2022F00019.md): Seat Track · corroded · Nov 12, 2021 · N782SP · Doug DC872 · Fuselage Main, Floor Beam
  > MAIN CABIN SEAT TRACK HAS CORROSION FROM STA. 1100-1120 BL 0". REF NRC# B000312.
- [SDR 2022F00018](https://openairdocs.org/sdr/2022F00018.md): Seat Track · corroded · Nov 11, 2021 · N782SP · Doug DC872 · Fuselage Main, Floor Beam
  > MAIN CABIN LWR SURFACE OF DOUBLE WIDE SEAT TRACK HAS CORROSION AT STA. 781 LBL 48. REF NRC# B000293.
- [SDR 2021F00365](https://openairdocs.org/sdr/2021F00365.md): None · none · Nov 5, 2021 · N782SP · Doug DC872 · Horizontal Stabilizer Structure
  > R/H HORZ. STAB L/E I/B SECTION LOWER SURFACE HAS CORROSION AROUND 2 FASTENERS BETWEEN STA. XFS. 122.500 & 128.750, REF NRC B000142.
- [SDR 2021FA0000324](https://openairdocs.org/sdr/2021FA0000324.md): Rib · cracked · Nov 4, 2021 · N782SP · Doug DC872 · Wing Structure
  > L/H WING O/B LOWER RIB A IS CRACKED AT STA. XFS.= 616.250, REF. NRC B000110
- [SDR E4EB20151115008](https://openairdocs.org/sdr/E4EB20151115008.md): Finger Doubler · broken · Nov 15, 2015 · N782SP · Doug DC872 · Fuselage Miscellaneous Structure
  > COCKPIT SUBFLOOR RT SIDE CUSP AREA STATION 148, FINGER DOUBLER HAS MANY BROKEN OFF FASTENERS.
- [SDR E4EB20151115007](https://openairdocs.org/sdr/E4EB20151115007.md): Seat Track · corroded · Nov 15, 2015 · N782SP · Doug DC872 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT, SEAT TRACK LUGS DAMAGED 2 PLACES STATION 834, LBL 24.
- [SDR E4EB20151115006](https://openairdocs.org/sdr/E4EB20151115006.md): Cap · corroded · Nov 15, 2015 · N782SP · Doug DC872 · Wing Miscellaneous Structure
  > LT WING INBD LE FUEL TANK UPPER TE TEE CAP HAS INTERGRANULAR CORROSION. BETWEEN XFS 30.000 - 57.000.
- [SDR E4EB20151115005](https://openairdocs.org/sdr/E4EB20151115005.md): Skin · corroded · Nov 15, 2015 · N782SP · Doug DC872 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB TIP HAS CORROSION ON SKIN AT STATIC WICK BASES.
- [SDR E4EB20151115004](https://openairdocs.org/sdr/E4EB20151115004.md): Skin · corroded · Nov 15, 2015 · N782SP · Doug DC872 · Wing, Plate/Skin
  > LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN STRINGER 9 & FWD SPAR, BETWEEN XRS 255 - 289.28-063.
- [SDR E4EB20151115003](https://openairdocs.org/sdr/E4EB20151115003.md): Skin · corroded · Nov 15, 2015 · N782SP · Doug DC872 · Wing, Plate/Skin
  > LT WING UPPER SURFACE HAS INTERGRANULAR CORROSION AROUND A FASTENER AT XRS763 & STRINGER 2 28-039.
- [SDR E4EB20151115002](https://openairdocs.org/sdr/E4EB20151115002.md): Rivet · cracked · Nov 15, 2015 · N782SP · Doug DC872 · Trailing Edge Flaps
  > LT INBD FLAP UPPER SURFACE INBD RUB PLATE HAS POPPED & CRACKED RIVETS 28-010.
- [SDR E4EB20151115001](https://openairdocs.org/sdr/E4EB20151115001.md): Seat Track · corroded · Nov 15, 2015 · N782SP · Doug DC872 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT SPLICE SAT 590, LBL 24.32-156.
- [SDR 2015FA0000537](https://openairdocs.org/sdr/2015FA0000537.md): Finger Doubler · corroded · Nov 2, 2015 · N721CX · Doug DC872 · Fuselage Main, Structure
  > COCKPIT SUBFLOOR FINGER DOUBLER AT LT SIDE OF CUSP BS 148 IS LIFTED UP DUE TO POSSIBLE CORROSION UNDERNEATH AND FASTENER IS LOOSE.
- [SDR E4EB2016F00009](https://openairdocs.org/sdr/E4EB2016F00009.md): Finger Doubler · corroded · Nov 2, 2015 · N721CX · Doug DC872 · Fuselage Miscellaneous Structure
  > COCKPIT SUBFLOOR FINGER DOUBLER AT LT SIDE OF CUSP WEB BS 148 IS LIFTED UP DUE TO POSSIBLE CORROSION UNDERNEATH AND FASTENER IS LOOSE.
- [SDR E4EB2015110200536](https://openairdocs.org/sdr/E4EB2015110200536.md): Skin · delaminated · Nov 2, 2015 · N721CX · Doug DC872 · Trailing Edge Flaps
  > RT WING OTBD FLAP, NR 4 VANE INBD UPPER SURFACE DENTED WITH DELAMINATION.
- [SDR E4EB2016F00008](https://openairdocs.org/sdr/E4EB2016F00008.md): Vane · delaminated · Nov 2, 2015 · N721CX · Doug DC872 · Trailing Edge Flaps
  > RT WING OTBD FLAP NR 4 FLAP VANE INBD UPPER SURFACE DENTED WITH DELAMINATION.
- [SDR E4EB2015110200535](https://openairdocs.org/sdr/E4EB2015110200535.md): Frame · corroded · Nov 2, 2015 · N782SP · Doug DC872 · Fuselage Main, Frame
  > FRAME BS 1060, UPPER CAP CORRODED INCLUDING EXFOLIATION AT SEVERAL PLACES FROM S34L TO S31R.
- [SDR E4EB2015113020](https://openairdocs.org/sdr/E4EB2015113020.md): Finger Doubler · damaged · Jun 8, 2015 · N782SP · Doug DC872 · Fuselage Miscellaneous Structure
  > COCKPIT SUBFLOOR RT CUSP AREA, STATION 148, FINGER DOUBLER HAS MANY BROKEN OFF FASTENERS. REMOVED DOUBLER FITTING & ATTACHMENT. FABRICATED TWO EACH FINGER DOUBLERS & INSTALLED IAW SRM.
- [SDR E4EB2015FA0000587](https://openairdocs.org/sdr/E4EB2015FA0000587.md): Fitting · corroded · Jun 7, 2015 · N782SP · Doug DC872 · Fuselage Main, Attach Fittings
  > NR A017107, AFT ACCESSORY COMPARTMENT S32R END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.
- [SDR E4EB2015FA0000586](https://openairdocs.org/sdr/E4EB2015FA0000586.md): Fitting · corroded · Jun 7, 2015 · N782SP · Doug DC872 · Fuselage Main, Attach Fittings
  > NR A017106, AFT ACCESSORY COMPARTMENT S34R END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.
- [SDR E4EB2015FA0000585](https://openairdocs.org/sdr/E4EB2015FA0000585.md): Fitting · corroded · Jun 7, 2015 · N782SP · Doug DC872 · Fuselage Main, Attach Fittings
  > AFT ACCESSORY COMPARTMENT S36 END FITTING AFT AFT SIDE OF FRAME FS 1530 IS CORRODED.
- [SDR E4EB2016111400002](https://openairdocs.org/sdr/E4EB2016111400002.md): Skin · corroded · May 31, 2015 · N782SP · Doug DC872 · Wing, Plate/Skin
  > LEFT WING UPPER SKIN HAS CORROSION AROUND FASTENERS AND VORTEX GENERATORS AT CENTER SPAR BETWEEN XW 408 AND XW 485.28-49.
- [SDR IXXA20120306007O](https://openairdocs.org/sdr/IXXA20120306007O.md): Battery · inoperative · Mar 14, 2012 · N721CX · Doug DC872 · Emergency Equipment
  > EMERGENCY FLASHLIGHT IN PASSENGER COMPARTMENT, INBD POSITION HAS WEAK BATTERY. R & R RECHARGEABLE EMERGENCY BATTERY IAW MM 33-50-1. OPS CHECKED GOOD.
- [SDR IXXA20110331002](https://openairdocs.org/sdr/IXXA20110331002.md): Longeron · corroded · Mar 31, 2011 · N721CX · Doug DC872 · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C-CHECK INSP FOUND AFT ACCESSORY COMPARTMENT LONGERON 23 RT CORRODED AT STA 1380.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW LONGERON SEGMENT AND SPLICERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS
- [SDR IXXA11SMN0062S](https://openairdocs.org/sdr/IXXA11SMN0062S.md): Fitting · cracked · Mar 31, 2011 · N721CX · Doug DC872 · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSP, FOUND AFT ACCESSORY COMPARTMENT AFT BATHTUB FITTING CRACKED AT STA 1530.000 LONGERON 34 LT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21 AND SRM 51-3-1.
- [SDR IXXA11SMN0055S](https://openairdocs.org/sdr/IXXA11SMN0055S.md): Skin · worn · Mar 26, 2011 · N721CX · Doug DC872 · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSP, FOUND LT OTBD FLAP UPPER SKIN WORN AT STA XF 169.000 - 213.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIRED PARTS IAW SRM CHAP 57-7-1, FIG 4 ITEM "C", DPS 4.710
- [SDR IXXA11SMN051S](https://openairdocs.org/sdr/IXXA11SMN051S.md): Fitting · cracked · Mar 25, 2011 · N721CX · Doug DC872 · Fuselage, Landing Gear Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND RT MLG WHEEL WELL FITTING CRACKED AT STATION 920, LONGERON 24 RT. REMOVED CRACKED FRAME FITTING. FABRICATED SPLICERS, SHIMS AND DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING AND REPAIR PART
- [SDR IXXA10SMN010S](https://openairdocs.org/sdr/IXXA10SMN010S.md): Skin · dented · Jan 9, 2010 · N721CX · Doug DC872 · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSP FOUND RT OTBD FLAP LOWER SKIN DENTED AT STA XF 380.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, P
- [SDR IXXA10SMN006S](https://openairdocs.org/sdr/IXXA10SMN006S.md): Skin · worn · Jan 9, 2010 · N721CX · Doug DC872 · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSP FOUND LT OTBD FLAP UPPER SKIN WORN AT STA XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PR
- [SDR IXXA10SMN003S](https://openairdocs.org/sdr/IXXA10SMN003S.md): Skin · deformed · Jan 9, 2010 · N721CX · Doug DC872 · Ailerons
  > DURING ROUTINE C CHECK INSP FOUND RT OTBD AILERON LOWER SKIN L/E DEFORMED AT STA XA 724.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE. FOUND WITH
- [SDR IXXA10SMN001S](https://openairdocs.org/sdr/IXXA10SMN001S.md): Skin · broken · Jan 6, 2010 · N721CX · Doug DC872 · Passenger/Crew Doors
  > DURING ROUTINE C CHECK INSP FOUND THE FWD PASSENGER DOOR OUTER SKIN UPPER PART EDGE BROKEN AND AFT UPPER CORNER DENTED. STRIPPED PAINT. REMOVED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED SKIN IAW SRM 52-3-2 FIGURE
- [SDR IXXA070037O](https://openairdocs.org/sdr/IXXA070037O.md): Wire · arced · Aug 5, 2007 · N721CX · Doug DC872 · Flight Control System Wiring
  > DURING APPROACH INTO KBWI, THE FLIGHT ATTENDANT NOTICED A FLASH AT THE CIRCUIT PANEL ABOVE THE RIGHT AFT SERVICE DOOR. THE CREW CONTINUED WITH THE APPROACH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND POWER WIRES CONTACTING LATCH OTHER BEHIND
- [SDR IXXA060610O](https://openairdocs.org/sdr/IXXA060610O.md): Cabin Pressure · unknown · Nov 25, 2006 · N721CX · Doug DC872 · Cabin Pressure Control System
  > AFTER TAKEOFF FROM RJTY, THE AIRCRAFT WOULD NOT PRESSURIZE. THE CREW RETURNED TO RJYT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AIR-CONDITIONING PACK SYSTEM AND PERFORMED AN OPERATIONAL CHECK OF THE AIRCRAFT PACK SYSTEM. THE AIRCRAFT S
- [SDR IXXA060604O](https://openairdocs.org/sdr/IXXA060604O.md): Selector Valve · out of adjust · Oct 1, 2006 · N721CX · Doug DC872 · Fuel Selector/Shut-Off Valve
  > DURING CRUISE FROM RJTY NUMBER ONE ENGINE FLAMED OUT AT FL340. THE CREW RETURNED TO RJTY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE, AND NO DEFECTS WERE FOUND. THE FUEL FILTER WAS REMOVED AND NO ABNORMAL CONTAMINATION WAS FOUND. NEW FUEL
- [SDR IXXA060603O](https://openairdocs.org/sdr/IXXA060603O.md): Engine · flamed out · Sep 28, 2006 · N721CX · Doug DC872 · Engine (Turbine/Turboprop)
  > DURING CLIMBOUT FROM RJTY AT FL390 NUMBER THREE ENGINE FLAMED OUT. THE CREW DESCENDED TO FL320 WITH IGNITERS IN BOTH AND OVERRIDE IN ALL ENGINES. APPROXIMATELY AT FL340 THE ENGINE RESTARTED, ALL INDICATIONS RETURNED TO NORMAL AND THE CREW CONTINUED THE FLIGH
- [SDR IXXA060600O](https://openairdocs.org/sdr/IXXA060600O.md): Engine · flamed out · Aug 25, 2006 · N721CX · Doug DC872 · Engine (Turbine/Turboprop)
  > DURING CRUISE FROM FJDG TO WSAP NR 2 ENGINE FLAMED OUT. THE CREW CONTINUED TO WSAP WHERE THEY LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE IAW ALL APPLICABLE DATA. NO DEFECTS WERE FOUND. THE FUEL FILTERS WERE INSPECTED, NO CONTAMINATION FOUND. NEW
- [SDR IXXA06SMN101S](https://openairdocs.org/sdr/IXXA06SMN101S.md): Vent · cracked · Mar 24, 2006 · N722CX · Doug DC872 · Vertical Stabilizer
  > DURING ROUTINE C-CHECK INSPECTION, REMOVED THE FWD BUFFET VENT TRIMMER VALVE AND PLUG OUTLET ON FUSELAGE. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7. REMOVED FWD BUFFET VENT TRIMMER VALVE IAW DC-8 MM 38-20-11 PAGES 201-202. REMOVED EXISTING INTERNAL DO
- [SDR IXXA06SMN067S](https://openairdocs.org/sdr/IXXA06SMN067S.md): Panel · displaced · Feb 24, 2006 · N722CX · Doug DC872 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, EO 25-DC8-520 R4 PARTITION UPPER ATTACHMENT RELOCATION TO FS-STC00171 LA-D. PERFORMED ALTERATION MAJOR IAW FAA FORM 8110-3 DATE 10-04-05. EO 25-DC-8-520 REV STATES 4 DATES 11-11-2005, ATI DWG C40-MO2 REV C DATE 10-04-05. F
- [SDR IXXA06SMN068S](https://openairdocs.org/sdr/IXXA06SMN068S.md): None · none · Feb 24, 2006 · N722CX · Doug DC872 · Standard Practices/Structures
  > DURING ROUTINE C-CHECK INSPECTION, ELT ANTENNA REMOVAL AND BLANKING PLATE INSTALLATION. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-06-06, ENGINEERING AUTHORIZATION AA71-2 REV IR DATE 01-24-06. REMOVED ELT ANTENNA IAW DC-8 MM 25-60-0 PAGE 201. FABRIC
- [SDR IXXA06SMN066S](https://openairdocs.org/sdr/IXXA06SMN066S.md): None · none · Feb 24, 2006 · N722CX · Doug DC872 · Standard Practices/Structures
  > DURING ROUTINE C-CHECK INSPECTION, EO 25-DC8-198 R9 INSTALL COMAT BOX. PERFORMED MAJOR ALTERATION IAW FAA FORM 8110-3 DATE 09-23-05, ATI DWG A95166-4 REV N DATE 09-23-05. INSTALLED COMAT BOX IAW ATI DWG 95166-4. COMPLIED WITH EO 25-DC8-198.
- [SDR IXXA06SMN065S](https://openairdocs.org/sdr/IXXA06SMN065S.md): Drain Mast · plugged · Feb 16, 2006 · N722CX · Doug DC872 · Waste Disposal System
  > DURING ROUTINE C-CHECK INSPECTION, INSTL; FWD LAV DRAIN MAST PLUG AT LOWER CENTER LINE. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-19-06, ATI DWG H74-102 REV B DATED 01-19-06, EO SEMAN 2006114 DATED 01-19-06. REMOVED EXISTING DRAIN MAST IAW DC8 SRM
- [SDR IXXA06SMN064S](https://openairdocs.org/sdr/IXXA06SMN064S.md): Repair · misinstalled · Feb 16, 2006 · N722CX · Doug DC872 · Aileron Control System
  > DURING ROUTINE C-CHECK INSPECTION, RT INBD AILERON SHOWS SEVERAL SPOTS OF CORROSION AND NON STANDARD REPAIR ON LWR PLATING, STA XA 550.000. PERFORMED MAJOR REPAIR. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED EXISTING PANEL PLATING (CORRODED) + REPAIR NO
- [SDR IXXA06SMN063S](https://openairdocs.org/sdr/IXXA06SMN063S.md): None · none · Feb 16, 2006 · N722CX · Doug DC872 · Aircraft Structures
  > DURING C CHECK, INSTALLATION OF DOUBLER ON FS 188.000 L-1 TO L-2R REQUIRED DUE TO SEXTANT EQUIPMENT REMOVAL. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06029 DATED 01-23-06, SEMAN DWG ED-4167 DATE 01-21-06, EO SEMAN # 2006100 DATE 01-23-06. REMOVED EXISTIN
- [SDR IXXA06SMN058S](https://openairdocs.org/sdr/IXXA06SMN058S.md): Fitting · corroded · Jan 26, 2006 · N722CX · Doug DC872 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPT- AFT SVC DOOR JAMB FITTING CORRODED, STA 1520.000 RBL 50. REMOVED CORROSION FROM FITTING IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW DC-8 S
- [SDR IXXA06SMN059S](https://openairdocs.org/sdr/IXXA06SMN059S.md): Pan · cracked · Jan 26, 2006 · N722CX · Doug DC872 · Leading Edge Devices
  > DURING ROUTINE C CHECK INSPECTION, RT WING CTR L/E, ZEE-PAN CRACKED 1" AT STA XS 526.000. REMOVED CRACKED ZEE PAN IAW DC8 SRM 51-1-20D ATI REPAIR SPECIFICATION NR 2003-05, DWG DOUGLAS NR 5769 857. PERFORMED HEAT TREATMENT IAW DC8 SRM 51-1-1 PAGES 1, 13, 17.
- [SDR IXXA06SMN062S](https://openairdocs.org/sdr/IXXA06SMN062S.md): Plug · installed · Jan 26, 2006 · N722CX · Doug DC872 · Fuselage Miscellaneous Structure
  > DURING C CHECK, 'LAVATORY DRAIN HOLE PLUG INSTALLATION REQUIRED (STA 240.000 - 260.000, L-19R TO L-18R). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06029 DATED 01-23-06, SEMAN DWG ED-4168 DATED 01-21-06, EO SEMAN NR 2006101 DATED 01-23-06. REMOVED EXISTIN
- [SDR IXXA06SMN061S](https://openairdocs.org/sdr/IXXA06SMN061S.md): None · none · Jan 26, 2006 · N722CX · Doug DC872 · Standard Practices/Structures
  > DURING C CHECK, 'FWD LAVATORY DRAIN HOLE PLUG INSTALLATION REQUIRED, STA 270.000 - 280.000, L-22R TO L-23R. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 1 (SHEET 1, 3). REMOVED FASTENERS IAW DC8 SRM 51-3-0. CUT OUT AREA, FABRICATED REPAIR DOUBLER, (02EA) I
- [SDR IXXA06SMN060S](https://openairdocs.org/sdr/IXXA06SMN060S.md): Repair · misinstalled · Jan 26, 2006 · N722CX · Doug DC872 · Aircraft Structures
  > DURING C CHECK, 'NON-STANDARD REPAIR ON FUSELAGE EXTERNAL SKIN (STA 1540.000 - 1550.000,L-17R TO L-19R. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 4, 5). REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTI
- [SDR IXXA06SMN057S](https://openairdocs.org/sdr/IXXA06SMN057S.md): Longeron · cracked · Jan 26, 2006 · N722CX · Doug DC872 · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, 'FWD ACCY COMPT- L-34R CRACKED BETWEEN STA 208.000 - STA 270.000. REMOVED CRACKED L-34R IAW DC-8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW LONGERON WITH RIVETS + HILOKS IAW DC-8 SRM

Next page: https://openairdocs.org/model/douglas-dc-8-72/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 = 'DC872'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-8-72/reports

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