# Service difficulty reports: Douglas DC-9-32F

A list on [Douglas DC-9-32F](https://openairdocs.org/model/douglas-dc-9-32f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 11 · 517 reports

- [SDR 2022F00149](https://openairdocs.org/sdr/2022F00149.md): Turbine Blades · damaged · Apr 30, 2021 · Doug DC932F · Engine (Turbine/Turboprop)
  > DURING THE CLIMB BETWEEN 12000 AND 15000 FT, A LOUD BANG WAS HEARD, OBSERVING PARAMETERS OF THE LEFT ENGINE OUT OF RANGE IN RELATION TO THE POSITION OF THE THROTTLE LEVER OF THE SAME ENGINE, PROCEEDING TO SHUTDOWN THE LEFT ENGINE PER QRH.
- [SDR 2022F00144](https://openairdocs.org/sdr/2022F00144.md): Warning Message · illuminated · Mar 30, 2021 · Doug DC932F · Cargo Compartments
  > INDICATION LOWER CARGO FIRE FOR ONE MINUTE.
- [SDR Y2PA201809250032](https://openairdocs.org/sdr/Y2PA201809250032.md): Skin Panel · corroded · Sep 25, 2018 · N208US · Doug DC932F · Fuselage Main, Plate/Skin
  > DURING C-CHECK AT KSFB, CORROSION WAS DISCOVERED ON SKIN AT STA 1114, LONGERON 18R. MAINTENANCE AT KSFB. REMOVED AND REPLACED LOWER SKIN FROM STA 1087-1121, LONGERON 18R-23R. REMOVED AND REINSTALLED MIDDLE SKIN FROM LONGERON 15R-18R. REMOVED AND REINSTALLED UP
- [SDR Y2PA2018092530030](https://openairdocs.org/sdr/Y2PA2018092530030.md): Pitot Tube · obstructed · Sep 23, 2018 · N205US · Doug DC932F · Pitot/Static System
  > CREW REPORTED 60 KNOT AIRSPEED DISCREPANCY DURING CLIMB. RAN COM 5.31.5 WITH NO SUCCESS. RETURNED TO KLRD AND DECLARED EMERGENCY. NO FURTHER INCIDENT. MAINTENANCE AT KLRD DISCONNECTED CAPT/FO’S PITOT LINES FROM PITOT TUBES. DURING INSPECTION PITOT OF TUBES FOU
- [SDR Y2PA201804170013](https://openairdocs.org/sdr/Y2PA201804170013.md): Control Panel · inoperative · Apr 15, 2018 · N205US · Doug DC932F · AC Generator-Alternator
  > ENCOUNTERED AN ELECTRICAL PROBLEM DURING CLIMB. RETURNED TO DEPARTURE. NO FURTHER ISSUES OCCURRED AND LANDED SAFELY. EMERGENCY DECLARED WITH ATC. LEFT GENERATOR OFF LIGHT ILLUMINATED DURING CLIMB. RAN COM PROCEDURE, NO HELP. APU DID NOT COME ONLINE. MAIN
- [SDR Y2PA2017112300031](https://openairdocs.org/sdr/Y2PA2017112300031.md): Sensor · failed · Nov 23, 2017 · N205US · Doug DC932F · Landing Gear Position and Warning
  > CREW REPORTED DURING GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. PERFORMED COM PROCEDURE, DECLARED EMERGENCY, REMAINED AIRBORNE TO BURN OFF FUEL TO MEET LANDING WEIGHT REQUIREMENTS. LANDING GEAR EXTENDED NORMALLY. COMPLETED UNEVENTFUL LANDI
- [SDR Y2PA2016092900024](https://openairdocs.org/sdr/Y2PA2016092900024.md): Warning System · malfunctioned · Sep 29, 2016 · N205US · Doug DC932F · Indicating/Recording System
  > IMMEDIATELY AFTER TAKEOFF, COULD SMELL AN ELECTRICAL BURNING ODOR FOLLOWED BY A MASTER CAUTION LIGHT. SEVERAL ANNUNCIATORS CAME ON AND OFF, FOLLOWED BY THE GPWS FAIL, STALL INDICATION FAIL AND FLAP/RUDDER/STOP INOPERATIVE REMAINING ON. IMMEDIATELY STARTED A
- [SDR Y2PA2016022800004](https://openairdocs.org/sdr/Y2PA2016022800004.md): Landing Gear · malfunctioned · Feb 25, 2016 · N208US · Doug DC932F · Landing Gear Position and Warning
  > DURING APPROACH, GEAR HANDLE PLACED IN DOWN POSITION. NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE GREEN. CYCLED GEAR, NOSE GEAR LIGHT STILL DID NOT ILLUMINATE GREEN. DECLARED EMERGENCY AND RAN COM EMERGENCY GEAR EXTENSION PROCEDURE. NOSE GEAR LIGHT STILL DID
- [SDR Y2PA2016011200001](https://openairdocs.org/sdr/Y2PA2016011200001.md): Skin · corroded · Jan 12, 2016 · N205US · Doug DC932F · Fuselage Main, Plate/Skin
  > MAINTENANCE DISCOVERED A MISSING RIVET FROM THE BELLY SKIN AT FS 585. UPON FURTHER INSPECTION, IT WAS DETERMINED THAT THERE WAS INTERNAL AND EXTERNAL CORROSION AND A TEMPORARY REPAIR WAS INSTALLED AND THE AIRCRAFT WAS FERRIED FOR REPAIR. MAINTENANCE INSTALLE
- [SDR K11A2013060616001](https://openairdocs.org/sdr/K11A2013060616001.md): Fuel Cap · missing · Jun 6, 2013 · N916CK · Doug DC932F · Fuel Storage
  > FUEL REPORTED AS VENTING FROM RT WING, NOTED FUEL IMBALANCE AND RETURNED TO DEPARTURE. UPON INVESTIGATION, FOUND RT OVERWING FUEL CAP MISSING, REPLACED CAP AND FUELED TO VTO, NO LEAKS NOTED.
- [SDR Y2PA20130511039](https://openairdocs.org/sdr/Y2PA20130511039.md): Line · failed · May 11, 2013 · N208US · Doug DC932F · Engine Oil Distribution (Airframe Furnished)
  > CREW REPORTED POST V1 & JUST INTO ROTATION, MASTER CAUTION ILLUMINATED FOR LT OIL PRESSURE LOW. DECISION MADE TO LEAVE MLG DOWN. OIL PRESSURE LOW & QTY DECREASING, NORMAL CHECKLIST COMPLETED & ABNORMAL CHECKLIST LEADING TO A PRECAUTIONARY SHUTDOWN. CREW
- [SDR Y2PA20130507036](https://openairdocs.org/sdr/Y2PA20130507036.md): Skin · cracked · May 6, 2013 · N208US · Doug DC932F · Trailing Edge Flaps
  > DURING C-CHECK INSPECTION AT YIP, MX DISCOVERED THE LT FLAP LOWER SKIN CRACKED. MX AT REPAIRED IAW SRM 57-01, FIGURE 3, SHEET 2 AND EA 96-51-02 R1.
- [SDR Y2PA20130507035](https://openairdocs.org/sdr/Y2PA20130507035.md): Hinge · cracked · May 6, 2013 · N208US · Doug DC932F · Trailing Edge Flaps
  > DURING C-CHECK INSPECTION, MX DISCOVERED THE LT WING CENTER AFT FLAP HINGE CRACKED. MX R & R HINGE IAW AMM 27-51-1 AND OHM 27-50-1.
- [SDR Y2PA20130507034](https://openairdocs.org/sdr/Y2PA20130507034.md): Bracket · corroded · May 6, 2013 · N208US · Doug DC932F · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, MX DISCOVERED THE MAIN UPPER CARGO DOOR LOWER SILL BRACKET CORRODED. MX R & R BRACKET IAW SRM 51-30-5.
- [SDR Y2PA20130507033](https://openairdocs.org/sdr/Y2PA20130507033.md): Panel · delaminated · May 6, 2013 · N208US · Doug DC932F · Wing, Plate/Skin
  > DURING C-CHECK INSPECTION, MX DISCOVERED THE INBD LT T/E WING PANEL DELAMINATED. MX R & R PANEL WITH SERVICEABLE IAW SRM 51-30-2.
- [SDR Y2PA20130507032](https://openairdocs.org/sdr/Y2PA20130507032.md): Panel · delaminated · May 6, 2013 · N208US · Doug DC932F · Wing, Plate/Skin
  > DURING C-CHECK INSPECTION, MX DISCOVERED THE SECOND FROM OTBD LT T/E WING PANEL DELAMINATED. MX R & R PANEL WITH SERVICEABLE IAW SRM 51-30-2.
- [SDR Y2PA20130507031](https://openairdocs.org/sdr/Y2PA20130507031.md): Tee Fitting · corroded · May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Attach Fittings
  > DURING C-CHECK INSPECTION, MX DISCOVERED A TEE FITTING CORRODED AT BS 160 ON THE RT CUSP LINE. MX R & R TEE FITTING IAW SRM 51-30-2 AND 51-30-5.
- [SDR Y2PA20130507030](https://openairdocs.org/sdr/Y2PA20130507030.md): Cusp Web · cracked · May 6, 2013 · Doug DC932F · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, MX DISCOVERED A CRACKED WEB AT STATION 953, LONGERON 18L. MX REPAIRED IAW SRM 53-01, FIGURE 2, SHEET 3 AND EA 96-51-02 R1.
- [SDR Y2PA20130507029](https://openairdocs.org/sdr/Y2PA20130507029.md): Longeron · corroded · May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION, MX DISCOVERED LONGERON END SHOVEL CORRODED IN THE LOWER AFT CARGO BAY AT BS 996 ON LONGERONS 29L. MX R & R SHOVELS IAW SRM 51-30-5.
- [SDR Y2PA20130507028](https://openairdocs.org/sdr/Y2PA20130507028.md): Sleeve · cracked · May 6, 2013 · N208US · Doug DC932F · Horizontal Stabilizer Structure
  > DURING C-CHECK INSPECTION, MX DISCOVERED BOTH LT AND RT HORIZONTAL STABILIZER HINGE BOLT SLEEVES CRACKED. MX R & R SLEEVES IAW AMM 55-10-0.
- [SDR Y2PA20130507027](https://openairdocs.org/sdr/Y2PA20130507027.md): Skin · corroded · May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, MX DISCOVERED THE LOWER AFT CARGO BAY SKIN CORRODED AT BS 756, LONGERON 27L 29R. MX REPAIRED IAW EA 13-53-321 AND DER DWG 53-13118-1, 8110-3, DATED 3/19/13.
- [SDR Y2PA20130507026](https://openairdocs.org/sdr/Y2PA20130507026.md): Web · corroded · May 6, 2013 · N208US · Doug DC932F · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, MX DISCOVERED THE LOWER AFT CARGO BAY CENTERLINE WEB CORRODED AT BS 996. MX REPAIRED IAW SRM 53-01, FIG 2 SHEET 3 AND EA 96-51-02 R3.
- [SDR Y2PA20130507025](https://openairdocs.org/sdr/Y2PA20130507025.md): Window Frame · cracked · May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Structure
  > DURING INSPECTION IAW AD 2002-21-09, 2 EACH.5" CRACKS WERE DISCOVERED IN THE CENTER FRAME OF THE COCKPIT WINDOW SILL. MX R & R THE COCKPIT WINDOW SILL CENTER FRAME WITH NEW IAW SB 53-290 R3, DWG SR09530268, SRM 51-30-2 AND 51-30-5.
- [SDR Y2PA20130507024](https://openairdocs.org/sdr/Y2PA20130507024.md): Spar · cracked · May 6, 2013 · N208US · Doug DC932F · Elevator, Spar/Rib
  > DURING C-CHECK X-RAY INSPECTION, MX DISCOVERED THE LT ELEVATOR FRONT SPAR CRACKED OUT OF LIMITS. MX AT YIP R & R THE LT ELEVATOR WITH A SERVICEABLE PART IAW MM 27-30-2.
- [SDR Y2PA20130306010](https://openairdocs.org/sdr/Y2PA20130306010.md): Skin · cracked · Mar 6, 2013 · N205US · Doug DC932F · Fuselage Main, Plate/Skin
  > EMERGENCY PROCEDURE, EMERGENCY DESCENT, UNSCHEDULED LANDING. FUSELAGE SKIN CRACKED AT BS 950 BETWEEN L14-15R, DISCOVERED DURING C-CHECK INSPECTION. MX REPAIRED IAW SRM 54-04, FIG 46.
- [SDR Y2PA20130306009](https://openairdocs.org/sdr/Y2PA20130306009.md): Shear Tie · cracked · Mar 6, 2013 · N205US · Doug DC932F · Fuselage Internal Mounting Structure
  > UNSCHEDULED LANDING, EMERGENCY DESCENT, ETC. SHEAR TIE CRACKED AT BS 945 BETWEEN LONGERONS 14R AND 17R, DISCOVERED DURING C-CHECK INSPECTION. MX REPLACED SHEAR TIE IAW SRM 51-30-5.
- [SDR Y2PA20130306008](https://openairdocs.org/sdr/Y2PA20130306008.md): Fitting · cracked · Mar 6, 2013 · N205US · Doug DC932F · Nacelle/Pylon, Attach Fittings
  > UNSCHEDULED LANDING, EMERGENCY DESCENT. RT PYLON REAR SPAR UPPER CAP FITTING AT STATION Y 1038 FOUND CRACKED DURING C-CHECK INSPECTION. MX REPLACED FITTING IAW SRM 51-30-1, 51-30-3 AND 51-30-5.
- [SDR Y2PA20130306007](https://openairdocs.org/sdr/Y2PA20130306007.md): Fitting · cracked · Mar 6, 2013 · N205US · Doug DC932F · Nacelle/Pylon, Attach Fittings
  > UNSCHEDULED LANDING, EMERGENCY DESCENT, ETC. LT PYLON REAR SPAR UPPER CAP FITTING AT STATION 1038 FOUND CRACKED DURING C-CHECK INSPECTION. MX REPLACED FITTING IAW SRM 51-30-1, 51-30-3 AND 51-30-5.
- [SDR Y2PA20130306006](https://openairdocs.org/sdr/Y2PA20130306006.md): Skin · chafed · Mar 6, 2013 · N205US · Doug DC932F · Vertical Stabilizer, Plate/Skin
  > EVIDENCE OF DAMAGE ON UPPER RT SIDE OF VERTICAL STABILIZER BETWEEN STATION ZV120 NEAR FORWARD END OF UPPER AND LOWER BODY FAIRINGS, DISCOVERED DURING C-CHECK. MX REPAIRED IAW DWG 55301301-1 AND APPROVED 8110-3 DATED 02/19/13.
- [SDR Y2PA20130306005](https://openairdocs.org/sdr/Y2PA20130306005.md): Attach Angle · cracked · Mar 6, 2013 · N205US · Doug DC932F · Nacelle/Pylon, Attach Fittings
  > EMERGENCY PROCEDURE, UNSCHEDULED LANDING, EMERGENCY DESCENT. RT PYLON UPPER PYLON TO FUSELAGE ATTACH ANGLE 12, AFT OF LEADING EDGE HAS 1 CRACK AT CORNER, DISCOVERED DURING C-CHECK INSPECTION. MX REPAIRED IAW SRM 54-04, FIG 10.
- [SDR Y2PA20120910041](https://openairdocs.org/sdr/Y2PA20120910041.md): Turbine Blades · damaged · Sep 10, 2012 · N205US · Doug DC932F · Turbine Section
  > CREW REPORTED AFTER DEPARTURE WHEN TRANSITIONING TO QUIET EPR POWER SETTING A SUDDEN LOUD AND EXTREME VIBRATION OCCURRED. OBSERVED LOSS OF EPR, N1 & N2. LT ENGINE WAS VERIFIED AS FAILING AND SOURCE OF VIBRATION WITH THROTTLE TO IDLE. EMERGENCY DECLARED AND
- [SDR Y2PA2011092000024](https://openairdocs.org/sdr/Y2PA2011092000024.md): Battery Pack · discharged · Sep 16, 2011 · N208US · Doug DC932F · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE DURING INSP. MX R & R BATTERY POWER SUPPLY IAW AMM 33-50-0. OPS CHECKS GOOD, NO OTHER DEFECTS NOTED.
- [SDR Y2PA2010111500028](https://openairdocs.org/sdr/Y2PA2010111500028.md): Downlock Switch · malfunctioned · Nov 10, 2010 · N208US · Doug DC932F · Landing Gear Position and Warning
  > UPON APPROACH, THE RT MLG DID NOT DISPLAY GREEN INDICATION, ONLY RED. CREW EXECUTED MISSED APPROACH AND REVIEWED COM PROCEDURES. CREW DIVERTED AND DECLARED AN EMERGENCY INBOUND. CREW FOLLOWED COM PROCEDURES FOR MANUAL EXTENSION OF GEAR AND SECONDARY SYS SHO
- [SDR ABXA080151](https://openairdocs.org/sdr/ABXA080151.md): Attach Angle · cracked · May 1, 2008 · N904AX · Doug DC932F · Fuselage Main, Attach Fittings
  > LEFT VERTICAL STAB ATTACH ANGLE CRACKED, LOCATED AT BASE OF RUDDER. REPAIRED LEFT VERTICAL STAB ATTACH ANGLE IAW DC9 SRM 53-05.
- [SDR ABXA080152](https://openairdocs.org/sdr/ABXA080152.md): Pan · cracked · May 1, 2008 · N904AX · Doug DC932F · Passenger/Crew Doors
  > MAIN ENTRY DOOR PAN CRACKED FORWARD SIDE (BOTTOM HINGE) SECOND STOP FROM BOTTOM. REMOVED AND REPAIRED DOOR IAW DC9 SRM.
- [SDR ABXA080150](https://openairdocs.org/sdr/ABXA080150.md): Skin · cracked · Apr 30, 2008 · N904AX · Doug DC932F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT STA 160, LONGERON 20 - 21 LEFT AT AIRSTAIR HINGE FORWARD SIDE. REPAIRED FUSELAGE SKIN CRACK IAW DC9 SRM.
- [SDR ABXA080120](https://openairdocs.org/sdr/ABXA080120.md): Relay · defective · Apr 5, 2008 · N909AX · Doug DC932F · Stabilizer Control System
  > PRIMARY TRIM CIRCUIT BREAKER TRIPPED WHILE SETTING TAKEOFF TRIM. WHILE MECHANIC WAS TROUBLESHOOTING PRIMARY TRIM, HEAVY SMOKE PRODUCED THROUGHOUT FRONT & REAR CABIN. CREW CONDUCTED EMERGENCY SHUT DOWN & EVACUATED AIRCRAFT. FOUND RELAY R20-15 BURNT. REPLACE
- [SDR ABXR080108](https://openairdocs.org/sdr/ABXR080108.md): Attach Angle · cracked · Mar 3, 2008 · N205US · Doug DC932F · Fuselage Miscellaneous Structure
  > ATTACH ANGLE FOR STA 41 TO STA 69 PRESSURE PANEL INTERCOSTAL CRACKED JUST RIGHT OF PLUG DOOR. REMOVED AND REPLACED ANGLES IAW DC9 SRM 51-30-5.
- [SDR ABXR080107](https://openairdocs.org/sdr/ABXR080107.md): Attach Angle · cracked · Mar 3, 2008 · N205US · Doug DC932F · Fuselage Miscellaneous Structure
  > ATTACH ANGLE FOR STA 41 TO STA 69 PRESSURE PANEL INTERCOSTAL CRACKED. SECOND INTERCOSTAL TO THE LEFT OF THE PLUG DOOR. REMOVED AND REPLACED IAW DC9 SRM 51-30-5.
- [SDR ABXR080106](https://openairdocs.org/sdr/ABXR080106.md): Fitting · cracked · Mar 3, 2008 · N205US · Doug DC932F · Nacelle/Pylon Miscellaneous Structure
  > PYLON UPPER REAR SPAR STRAP CLIP JUST INSIDE PYLON CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW CLIP IAW DC9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXR080105](https://openairdocs.org/sdr/ABXR080105.md): Attach Angle · cracked · Mar 2, 2008 · N205US · Doug DC932F · Fuselage Main, Keel
  > LEFT WHEEL WELL KEEL WEB UPPER ATTACH ANGLE AT STA 718 CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXR080104](https://openairdocs.org/sdr/ABXR080104.md): Attach Angle · cracked · Feb 29, 2008 · N205US · Doug DC932F · Fuselage Main, Bulkhead
  > INBOARD BULKHEAD STA 718 ATTACH ANGLE CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXR080103](https://openairdocs.org/sdr/ABXR080103.md): Skin · cracked · Feb 28, 2008 · N205US · Doug DC932F · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR SKIN CRACKED AT DOOR HANDLE. REPAIRED DOOR IAW DC9 SRM 52-05, FIGURE 30, SHEET 1.
- [SDR ABXR080102](https://openairdocs.org/sdr/ABXR080102.md): Skin · cracked · Feb 28, 2008 · N205US · Doug DC932F · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR SKIN CRACKED AT DOOR HANDLE. REPAIRED AND PAINTED IAW DC9 SRM 25-05 AND 51-10.
- [SDR ABXA070425](https://openairdocs.org/sdr/ABXA070425.md): Battery Pack · defective · Dec 11, 2007 · N904AX · Doug DC932F · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW DC9 AMM CHAPTER 33.
- [SDR ABXA070424](https://openairdocs.org/sdr/ABXA070424.md): Battery · discharged · Dec 8, 2007 · N905AX · Doug DC932F · Emergency Lighting
  > CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.
- [SDR Y2PA200700026](https://openairdocs.org/sdr/Y2PA200700026.md): Csd · failed · Nov 2, 2007 · N208US · Doug DC932F · Engine (Turbine/Turboprop)
  > CREW REPORTED ENGINE VIBRATION THEN FAILURE ON NR 2 ENGINE. IRREGULARITY FILLED OUT BY CREW REPORTED AS FOLLOWS. AFTER DEPARTURE IN CLIMB, VIBRATION FOLLOWED BY NR 2 ENGINE FLAME OUT AT FL190 FOLLOWED BY AIRCRAFT CROSSTIE LOCKOUT. CREW DECLARED AN EMERGENCY
- [SDR ABXA070262](https://openairdocs.org/sdr/ABXA070262.md): Frame · cracked · Aug 15, 2007 · N909AX · Doug DC932F · Fuselage Main, Frame
  > WHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME, REF AD 2002-21-09. REPLACED FRAME IAW DC9 SRM 51-30-02 AND 51-30-05.
- [SDR ABXA070264](https://openairdocs.org/sdr/ABXA070264.md): Angle · cracked · Aug 15, 2007 · N909AX · Doug DC932F · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH EA 53300036, FOUND CRACKED ANGLE, REF AD 2002-21-09. REPLACED ANGLE IAW DC9 SRM 51-30-05.
- [SDR ABXA070263](https://openairdocs.org/sdr/ABXA070263.md): Bracket · cracked · Aug 15, 2007 · N909AX · Doug DC932F · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH EA 53300036, FOUND CRACKED BRACKET, REF AD 2002-21-09. REPLACED BRACKET IAW DC9 SRM 51-30-02 AND 51-30-05.

Next page: https://openairdocs.org/model/douglas-dc-9-32f/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 = 'DC932F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-9-32f/reports

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