# Service difficulty reports: Douglas DC-8-73F

A list on [Douglas DC-8-73F](https://openairdocs.org/model/douglas-dc-8-73f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 310 · 15,471 reports

- [SDR E4EB2015112401](https://openairdocs.org/sdr/E4EB2015112401.md): Frame · cracked · May 28, 2015 · N782SP · Doug DC873F · Fuselage Main, Frame
  > EXTERIOR FUSELAGE AFT LT LAVATORY, SERVICE PANEL CUT OUT WORN & GOUGED AT LATCH CONTACT POINTS. FOUND GOUGE TO BE OUT OF LIMITS & FOUND CRACK ON FRAME. REPAIRED IAW SRM.
- [SDR IXXA20121215035O](https://openairdocs.org/sdr/IXXA20121215035O.md): Warning Light · false activation · Dec 15, 2012 · N604BX · Doug DC873F · Door Warning System
  > DURING TAKEOFF, BELLY DOOR OPEN LIGHT ILUMINATED. TAKEOFF WAS ABORTED. RESET ALL CARGO DOORS IAW MM 52-70-0 ALL WARNING LIGHTS OUT.
- [SDR IXXA20121127032O](https://openairdocs.org/sdr/IXXA20121127032O.md): Connector · loose · Nov 27, 2012 · N606AL · Doug DC873F · Landing Gear System Wiring
  > ON APPROACH, RT MLG DOWN GREEN LIGHT DID NOT ILLUMINATE, NO RED LIGHTS ILLUMINATED. CYCLED LANDING GEAR AND GREEN LIGHT ILLUMINATED. RESEATED CONNECTOR PLUG ON RT MLG DOWNLOCK SWITCH IAW MM 32-60-0. OPS CHECKS GOOD.
- [SDR DHLA20120413006](https://openairdocs.org/sdr/DHLA20120413006.md): Battery Pack · inoperative · Apr 13, 2012 · N873SJ · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. ACFT WAS GROUNDED. R & R EMERGENCY LIGHT BATTERY PACK. OPS CHECKED GOOD IAW MM 33-50-0.
- [SDR DHLA201200005](https://openairdocs.org/sdr/DHLA201200005.md): Warning Light · false activation · Apr 5, 2012 · N806DH · Doug DC873F · Engine Thrust Reverser
  > ON CLIMB OUT, NR 4 THRUST REVERSER LIGHT ILLUMINATED. RAN THRUST REVERSER EMERGENCY STOW CHECKLIST. LIGHT REMAINED ILLUMINATED. RAN ABNORMAL IN FLIGHT ENGINE SHUTDOWN AND SHUTDOWN ENGINE. WINDMILLED OIL PRESSURE JUST ABOVE 0 PSI AND SHUTDOWN FOR APROX 10 M
- [SDR DHLA201203140004](https://openairdocs.org/sdr/DHLA201203140004.md): Cap · loose · Mar 14, 2012 · N806DH · Doug DC873F · Turbine Engine Oil System
  > NR 4 ENGINE SHUTDOWN DURING FLIGHT WITH OIL QTY AT 2 QUARTS. ACFT WAS GROUNDED. INSPECTED ENGINE FOUND OIL CAP TO BE LOOSE INSTALLED NEW CAP ASSY IAW MM 79-11-10 OIL IAW MM 12-10-00 INSPECTED CHIP DETECTOR IAW MM 79-00-00 NO DEFECTES NOTED RAN NR 4 ENGINE IA
- [SDR IXXA20120306006S](https://openairdocs.org/sdr/IXXA20120306006S.md): Radome · damaged · Mar 5, 2012 · N603AL · Doug DC873F · Aerodynamic Fairings
  > NOSE RADOME DAMAGED. R & R NOSE RADOME IAW MM 53-50-1.
- [SDR IXXA20120223004S0](https://openairdocs.org/sdr/IXXA20120223004S0.md): Door · out of rig · Feb 23, 2012 · N604BX · Doug DC873F · Passenger/Crew Doors
  > L1 DOOR OUT OF RIG. R & R L1 DOOR AND ADJUSTED TO OPENING IAW MM 52-11-1, OPS CHECKED GOOD.
- [SDR DHLA201200003](https://openairdocs.org/sdr/DHLA201200003.md): Blade · missing · Jan 31, 2012 · N803DH · Doug DC873F · Turbine Section
  > NR 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 A
- [SDR DHLA2012010600001](https://openairdocs.org/sdr/DHLA2012010600001.md): Fire Detector · malfunctioned · Jan 6, 2012 · N803DH · Doug DC873F · Fire Detection
  > NR 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 FIRE
- [SDR DHLA20120106002](https://openairdocs.org/sdr/DHLA20120106002.md): Battery Pack · inoperative · Jan 6, 2012 · N806DH · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. ACFT GROUNDED. R & R EMERGENCY LIGHTS BATTERY PACK IAW MM 33-50-0 WORKING NORMAL.
- [SDR IXXA110082O](https://openairdocs.org/sdr/IXXA110082O.md): Connector · loose · Dec 21, 2011 · N602AL · Doug DC873F · Landing Gear System Wiring
  > DURING UPLATCH CHECK, DOOR NOT LATCH LIGHT CAME ON. THE CREW CYCLED MAIN GEARS TWICE AND DOOR NOT LATCH LIGHT REMAINED ON. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MAIN GEAR DOORS AND FOUND THE LT GEAR DOOR SWITCH CONNECTOR LOOSE AND DIRTY. M
- [SDR IXXA110081O](https://openairdocs.org/sdr/IXXA110081O.md): Connector · dirty · Dec 20, 2011 · N602AL · Doug DC873F · Landing Gear System Wiring
  > DURING CLIMB OUT, AFTER GEAR RETRACTION, DOOR NOT LATCH LIGHT REMAINED ON. CREW CYCLED MAIN GEAR AND LIGHT REMAINED ON. LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MAIN GEAR DOOR UPLATCH SWITCHES AND FOUND THE RT MAIN GEAR DOOR SWITCH CONNECTOR DIRTY. CLEA
- [SDR DHLA201100539](https://openairdocs.org/sdr/DHLA201100539.md): Actuator · leaking · Nov 15, 2011 · N807DH · Doug DC873F · Landing Gear Actuator
  > AFTER DEPARTURE, ACFT LOST HYDRAULIC LEVEL TO JUST ABOVE THE EMERGENCY LEVEL. ALL PROCEDURES COMPLIED AND ACFT RETURNED TO DEPARTURE. ACFT GROUNDED ON ARRIVAL. R & R RT MLG ACTUATOR AND REPLENISHED HYDRAULICS IAW MM 37-32-2, & 12-03-00.
- [SDR IXXA110072O](https://openairdocs.org/sdr/IXXA110072O.md): Engine · failed · Oct 27, 2011 · N604BX · Doug DC873F · Engine (Turbine/Turboprop)
  > DURING TAKEOFF ROLL NR 2 ENGINE COMPRESSOR STALLED 3 TIMES. ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. FOUND N1 SEIZED. REPLACED NR 2 ENGINE IAW J/C 7004, 7005, 7104, AND 7104. RAN ENGINE IAW ERH 70.01. OPS CHECKED GOOD. REJECTED TAKEO
- [SDR DHLA201100538](https://openairdocs.org/sdr/DHLA201100538.md): Battery Pack · inoperative · Oct 6, 2011 · N806DH · Doug DC873F · Emergency Lighting
  > DURING PREFLIGHT FOUND EMERGENCY EXIT LIGHTS ARMED-NO POWER ON ACFT BATTERY DEAD. ACFT WAS GROUNDED. R & R EMERGENCY LIGHT BATTERY RACK ASSY IAW MMS 33-50-00. OPS CK-NORMAL.
- [SDR IXXA110060O](https://openairdocs.org/sdr/IXXA110060O.md): Engine · slow · Sep 11, 2011 · N605AL · Doug DC873F · Engine (Turbine/Turboprop)
  > REJECTED TAKEOFF DUE TO ASSYMETRICAL THRUST ON TAKEOFF ROLL. THE NR 4 ENGINE SLOW TO ACCELERATE, DID NOT REACH MAX POWER. THE CREW RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX PREFORMED ACCELERATION CHECK, OPS CHECKED GOOD IAW ERH 72.01.1. PREFORMED REJE
- [SDR DHLA201100537](https://openairdocs.org/sdr/DHLA201100537.md): Skin · corroded · Aug 26, 2011 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE HAS CRACK IN SKIN AT STA 100 AT LONGERON 35 & 36R. CRACK IS PROBABLY INDUCED BY CORROSION. COMPLIED WITH STEPS 1-11 OF EVA D853-00412. FABRICATED FILLER, DOUBLER AND INSTALLED REPAIR. MAJOR REPAIR
- [SDR DHLA2011F00187](https://openairdocs.org/sdr/DHLA2011F00187.md): Skin · cracked · Aug 25, 2011 · N804DH · Doug DC873F · Fuselage Main, Plate/Skin
  > WHILE COMPLYING WITH VISUAL WALK AROUND INSP, A CRACK WAS FOUND IN THE LOWER FUSELAGE SKIN AT STA 100.5. UPON FURTHER INVESTIGATION THE CAUSE OF THE CRACK WAS CORROSION. THE CRACK WAS ADJACENT TO ANOTHER REPAIR WHICH WAS REMOVED AND THE NEW REPAIR INCOORPERA
- [SDR DHLA201100536](https://openairdocs.org/sdr/DHLA201100536.md): Battery Pack · inoperative · Aug 15, 2011 · N802DH · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOPERATIVE. ACFT GROUNDED. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AND OPS CHECKED GOOD IAW MM 33-50-1.
- [SDR DHLA201100534](https://openairdocs.org/sdr/DHLA201100534.md): Engine · failed · Jul 28, 2011 · N806DH · Doug DC873F · Engine (Turbine/Turboprop)
  > DURING DESCENT NR3 ENGINE AT IDLE, STARTED RUMBLING ENGINE N1 & N2 SPOOLED DOWN NO- OIL PRESSURE. ACFT WAS GROUNDED. REPLACED NR 3 ENGINE ASSY.
- [SDR DHLA201100533](https://openairdocs.org/sdr/DHLA201100533.md): Line · leaking · Jul 26, 2011 · N806DH · Doug DC873F · Engine (Turbine/Turboprop)
  > AT FL 380 ENGINE NR 1 FAILED. COMPLETED ENGINE FAILURE CHECK LIST. TRIED RESTART AT 340 NO GOOD. AT FL 220 RESTART SUCCESSFUL. ALL PARAMETERS NORMAL. ACFT WAS GROUNDED UPON ARRIVAL AT CVG. PERFORMED MM TS CHART 71-00-00FAULT 51. CHECKED SPECIFIC GRAVITY WAS.
- [SDR DHLA201100525](https://openairdocs.org/sdr/DHLA201100525.md): Battery · inoperative · Jul 11, 2011 · N806DH · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ONLY STAY ON FOR A FEW SECONDS. ACFT WAS GROUNDED. REPLACED EMERGENCY EXIT LIGHT BATTERY ASSY AND SYS. OPS CK GOOD IAW MM 33-50-1.
- [SDR IXXA110049O](https://openairdocs.org/sdr/IXXA110049O.md): Damper · defective · Jun 27, 2011 · N605AL · Doug DC873F · Elevator Control System
  > DURING CLIMB OUT, THE CREW NOTICED AT 250 KNOTS A PULSING IN BOTH CONTROL COLUMNS. THE PULSE INCREASED THROUGH ANY PITCH CHANGE WHETHER USING THE AUTOPILOT OR MANUALLY FLYING THE ACFT (MORE NOTICEABLE PULSE). THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDEN
- [SDR DHLA201100531](https://openairdocs.org/sdr/DHLA201100531.md): Fitting · corroded · Jun 23, 2011 · N807DH · Doug DC873F · Wing, Attach Fittings
  > RT OUTER WING FWD BOTTOM PANEL.- FITTING HAS EXFOLIATION CORROSION S-62 (NR 4 ALT TANK) STA XW 408.000 PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, DWG 3640143. REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0, PG 16, FIG 7
- [SDR DHLA201100530](https://openairdocs.org/sdr/DHLA201100530.md): Fitting · corroded · Jun 23, 2011 · N807DH · Doug DC873F · Wing, Attach Fittings
  > RT OUTER WING FWD BOTTOM PANEL.- FITTING HAS EXFOLIATION CORROSIOIN S-63, STA XW 408.000 (NR4 ALT TANK) PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, DWG 3640143. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16, FIG
- [SDR DHLA201100516](https://openairdocs.org/sdr/DHLA201100516.md): Battery Pack · inoperative · Jun 22, 2011 · N805DH · Doug DC873F · Emergency Lighting
  > DURING PDC CK FOUND EMERGENCY LIGHTS INOPERATIVE. ACFT WAS GROUNDED. R & R EMER LIGHTS BATTERY PACK IAW MMS 33-50-10. OPS-CK-GOOD.
- [SDR IXXA110048O](https://openairdocs.org/sdr/IXXA110048O.md): Connector · dirty · Jun 10, 2011 · N606AL · Doug DC873F · Light System Wiring
  > ON FINAL APPROACH WITH LANDING GEAR LEVER DOWN, RT LANDING LIGHT DID NOT ILLUMINATE. THE CREW CYCLED THE GEAR AND GEAR LIGHT ILLUMINATED 10 SECONDS AFTER GEAR CYCLE. THEY LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND CLEANED THE CONNECTOR PLUG ON THE DOWN
- [SDR DHLA201100532](https://openairdocs.org/sdr/DHLA201100532.md): Stringer · cracked · Jun 7, 2011 · N807DH · Doug DC873F · Wing, Longeron/Stringer
  > RT INNER WING AFT TOP PANEL.- STRINGER NR4 CRACKED STA XRS 87.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 07-21-11, EVA D857-00408 REV IR DATED 07-06-11. CUT OUT DAMAGED STRINGER SEGMENT, FABRICATED SPLICES & NEW STRINGER SEGMENT IAW DWG ED-5386 D
- [SDR DHLA201100527](https://openairdocs.org/sdr/DHLA201100527.md): Longeron · corroded · Jun 7, 2011 · N807DH · Doug DC873F · Fuselage Main, Longeron/Stringer
  > FWD ACCY COMPT- L33R SHOWS EXFOLIATION CORROSION AT STA 14.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 10 SHEET 1,3, TR 53-153 SHEET 4, TR 53-193. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMIT
- [SDR DHLA201100521](https://openairdocs.org/sdr/DHLA201100521.md): Longeron · corroded · Jun 7, 2011 · N807DH · Doug DC873F · Fuselage Main, Longeron/Stringer
  > FWD ACCY COMPT- L33R SHOWS EXFOLIATION CORROSION AT STA 14.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 10 SHEET 1,3, TR 53-153, SHEET 4, TR 53-193. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS
- [SDR DHLA201100515](https://openairdocs.org/sdr/DHLA201100515.md): Amplifier · inoperative · Jun 7, 2011 · N806DH · Doug DC873F · Smoke Detection
  > AMBER CARGO SMOKE LIGHT ILLUMINATED DURING DESCENT, LIGHT EXTINGUISHED ON SHORT FINAL APPROACH TO LANDING, NO SMOKE OR FIRE WAS NOTICED TO CREW. EMERGENCY WAS DECLARED. ACFT WAS GROUNDED
- [SDR DHLA201100524](https://openairdocs.org/sdr/DHLA201100524.md): Frame · deformed · Jun 6, 2011 · N807DH · Doug DC873F · Fuselage Main, Frame
  > MAIN CARGO BAY FRAME DEFORMED BS 1580.000 L19TO 21R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 6, SRM 53-4-1 FIG. 51 SHEET 21. REMOVED DEFORMED FRAME SEGMENT & EXISTING ANGLES IAW SRM 51-1-20D. FABRICATED NEW SEGMENT IAW SRM 53-4-1 FIG. 51 SHEET 21 I
- [SDR DHLA201100523](https://openairdocs.org/sdr/DHLA201100523.md): Fitting · corroded · Jun 6, 2011 · N807DH · Doug DC873F · Fuselage Main, Attach Fittings
  > FWD ACCY COMPT FITTING CORRODED BY EXFOLIATION STA 8.000 L33R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 FOUND WITHIN LIMITS IAW SRM 53-2-0, PG 2P. REMOVED CORRODED FITING IAW SRM 51-1-20 D SRM 51-3-0. CLEANE
- [SDR IXXA110046O](https://openairdocs.org/sdr/IXXA110046O.md): Link · failed · Jun 5, 2011 · N604BX · Doug DC873F · Landing Gear Door Retract Section
  > AFTER TAKEOFF, THE CREW HEARD A LOUD NOISE FROM NOSE GEAR AREA, THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX FOUND RT NOSE GEAR DOOR OPENED, NO FURTHER DEFECTS NOTED. THEY REPLACED RT FWD NOSE GEAR LINK. OPS CHECK GOOD IAW MM 32-22-1. ACFT WAS RE
- [SDR IXXA110045O](https://openairdocs.org/sdr/IXXA110045O.md): Latch · failed · Jun 5, 2011 · N604AL · Doug DC873F · Landing Gear Doors
  > AFTER TAKEOFF, THE CREW HEARD A LOUD NOISE FROM NOSE GEAR AREA, THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED NOSE GEAR AND FOUND RT NOSE GEAR DOOR OPENED. THEY CLOSED AND SECURED DOOR LOCK MECHANISM DOOR. OPS CHECK GOOD IAW MM 32-22-1.
- [SDR DHLA201100529](https://openairdocs.org/sdr/DHLA201100529.md): Tee Fitting · cracked · Jun 3, 2011 · N807DH · Doug DC873F · Service Doors
  > R2 SERVICE DOOR INNER FITTING CRACKED 1". REMOVED CRACKED TEE FITTING IAW SRM 51-1-20D, SRM 51-1-21. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TEE FITTING IAW SRM 51-1-20D, SRM 51-1-21, SRM 51-3-1.
- [SDR DHLA201100520](https://openairdocs.org/sdr/DHLA201100520.md): Skin · corroded · Jun 2, 2011 · N807DH · Doug DC873F · Fuselage Main, Plate/Skin
  > EXT FUS LWR SKIN CORRODED STA 1460.000 - 1480.000, L34L TO 35L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1, SRM 53-4-1, FIG. 17A SHEET 2. REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2M. REMOVED CORRODED PLATING
- [SDR DHLA201100522](https://openairdocs.org/sdr/DHLA201100522.md): Skin · cracked · Jun 1, 2011 · N807DH · Doug DC873F · Wing, Plate/Skin
  > RT WING UPPER SKIN 2" CRACK STA XRS 74.869 (BETWEEN CTR SPAR AND S-8). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-28-11, EVA D857-00406 REV IR, ASTAR DWG ES D85700406-001-D REV "B". CUT OUT DAMAGED AREA & FABRICATED FILLER PLATE & REPAIR DOUBLER IAW
- [SDR DHLA201100519](https://openairdocs.org/sdr/DHLA201100519.md): Frame · deformed · Jun 1, 2011 · N807DH · Doug DC873F · Fuselage Main, Frame
  > MAIN CARGO COMPT FRAME DEFORMED STA 1580.000 L21 TO 19L PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2, SHEET 6, SRM 53-4-1 FIG 51 SHEET 21. REMOVED DEFORMED FRAME SEGMENT & EXISTING ANGLES IAW SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT IAW SRM 53-4-1 FIG 51, SHE
- [SDR DHLA201100528](https://openairdocs.org/sdr/DHLA201100528.md): Angle · cracked · May 31, 2011 · N807DH · Doug DC873F · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENG TO PYLON ANGLE CRACK 10" STA YN 183.000 AT 12 O'CLOCK POS, LT SIDE. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATE 07-02-11, EVA D854-00407, REV IR DATED 06-14-11, DWG ASTAR ES D85400407-001-D. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D, SRM 5
- [SDR DHLA201100526](https://openairdocs.org/sdr/DHLA201100526.md): Fitting · corroded · May 31, 2011 · N807DH · Doug DC873F · Fuselage, Landing Gear Attach Fittings
  > RT MLG WHEEL WELL FITTING CORRODED AT STA 857.125, RBL 47 (EXFOLIATION). REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-20. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2M. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8
- [SDR DHLA201100518](https://openairdocs.org/sdr/DHLA201100518.md): Skin · corroded · May 31, 2011 · N807DH · Doug DC873F · Ailerons
  > RT AILERON SKIN LOWER PLATING CORRODED STA XA 737.000 - XA 775.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4. REMOVED LEVEL 2 CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 FIG. 7. REMOVED CORRODED PANEL PLATING IAW SRM 57-1-0 PG 1
- [SDR IXXA110043O](https://openairdocs.org/sdr/IXXA110043O.md): Lock Sensor · defective · May 30, 2011 · N605AL · Doug DC873F · Engine Thrust Reverser
  > AFTER TAKEOFF, NR 2 THRUST REVERSER LIGHT WAS BLINKING. THE CREW ACTUATED THE EMERGENCY STOW PUMP BUT NO HELP. THEY RETURNED TO DEPARTURE AND UPON LANDING THE LIGHT WENT OUT. MX TROUBLESHOT THE THRUST REVERSER SYS AND FOUND RT UPPER AND LOWER THRUST REVERSE
- [SDR IXXA110040O](https://openairdocs.org/sdr/IXXA110040O.md): Fuel Control · out of adjust · May 12, 2011 · N604BX · Doug DC873F · Fuel Control/Turbine Engines
  > DURING CRUISE, NR 4 ENGINE FLAMEDOUT. THE CREW ATTEMPTED RESTART, ENGINE WOULD NOT START. THEY LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FAULT TREE 51, CHANGED NR 4 FUEL FILTER, RAN ENGINE AND FOUND FLIGHT IDLE LOW, ADJUSTED FLIGHT IDLE. OPS CHECK GOO
- [SDR DHLA201100500](https://openairdocs.org/sdr/DHLA201100500.md): Battery Pack · inoperative · May 7, 2011 · N873SJ · Doug DC873F · Emergency Lighting
  > EMERGENCY BATTERY PACK DEAD. ACFT WAS GROUNDED. R & R EMERGENCY BATTERY PACK IAW MM 33-50-1. GROUND CKS GOOD.
- [SDR IXXA110037O](https://openairdocs.org/sdr/IXXA110037O.md): Control Tube · dirty · May 5, 2011 · N602AL · Doug DC873F · Engine (Turbine/Turboprop)
  > AT FLIGHT LEVEL 370, THE NR 2 ENGINE POWER ROLLED BACK FROM 94 PERCENT TO 87 PERCENT WITH A CORRESPONDING DROP IN EGT AND N2. THE PMC FOR NR 2 ENGINE WAS SWITCH OFF AND NR 2 ENG ROLLED DOWN MORE TO 50 PERCENT N1 AND 400 DEGREE EGT. THE CREW SHUTDOWN NR 2 ENGIN
- [SDR DHLA201100049](https://openairdocs.org/sdr/DHLA201100049.md): Battery Pack · discharged · May 4, 2011 · N806DH · Doug DC873F · Emergency Lighting
  > ALL 3 EMERGENCY EVAC LIGHTS DO NOT ILLUMINATE OR ARE VERY DIM WHEN PERFORMING A BATTERY CHECK. ACFT WAS GROUNDED. R & R EMERGENCY LIGHTS BATTERY RACK ASSY IAW DC8 33-50-1, OPS CK OK.
- [SDR DHLA201100041](https://openairdocs.org/sdr/DHLA201100041.md): Skin · corroded · May 1, 2011 · N806DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BULGING AND CRACKED AT FS 26.0, BETWEEN LONGERONS 35L AND 36. ACCOMPLISHED SKIN EXTERNAL DOUBLER REPAIR IAW EVA D853-0041 REV A, DWG D85300441-001-D, REV D, AND SRM 53-2-1, FIG 8. REF NR 10081-10 UNDER W/O 10081. REPAIR LOCATIONS LISTED BELOW.
- [SDR DHLA201100048](https://openairdocs.org/sdr/DHLA201100048.md): Skin · cracked · Apr 11, 2011 · N805DH · Doug DC873F · Ailerons
  > LT OTBD AIL LWR NOSE PLATING CRACKED 1" STA XA 734.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0, PG 1, SRM 57-8-1, FIG 4. REMOVED DAMAGED NOSE PLATING IAW SRM 57-1-0, PG 1, SRM 51-1-21. FABRICATED NEW NOSE PLATING IAW SRM 57-8-1, FIG 4, ITEM "H". CLEANED, TRE

Next page: https://openairdocs.org/model/douglas-dc-8-73f/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 = 'DC873F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-8-73f/reports

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