# Service difficulty reports: Douglas DC-9-33F

A list on [Douglas DC-9-33F](https://openairdocs.org/model/douglas-dc-9-33f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 34 · 1,681 reports

- [SDR FXGA202106262124](https://openairdocs.org/sdr/FXGA202106262124.md): Frame · damaged · Jun 26, 2021 · N935CE · Doug DC933F · Fuselage Main, Frame
  > OUT OF LIMIT GAUGE ON S/STA 180 FRAME AT STRINGER 24R. TO REPAIR A FUSELAGE FRAME WITH OUT OF LIMIT GAUGE. CUT OUT DAMAGE AND INSTALL REPAIR PARTS PER DC-9/MD-80 SRM 53-03 FIGURE 4. MAINTENANCE REQUIREMENTS: NORMAL MAINTENANCE, SEE PAGE 4 FOR DEATAILS.
- [SDR 2022F00150](https://openairdocs.org/sdr/2022F00150.md): Wheel · misinstalled · May 29, 2021 · Doug DC933F · Landing Gear System
  > LEAVING RUNWAY 11 AT MTY ON DRIVE E ANTISKID LIGHT TILLED FOR ONE SECOND, AFTER PARKING AT PLATFORM WE WERE NOTICED THAT LH MAIN LANDING GEAR WHEEL NBR 1 WAS MISSING.
- [SDR 2022F00158](https://openairdocs.org/sdr/2022F00158.md): None · none · Sep 2, 2020 · Doug DC933F · Landing Gear Steering System
  > DURING TAKE OFF ON RUNWAY 27, AT 40-60 KTS APROX. AIRCRAFT DRIFLED TO THE RIGHT, WE TRIED TO CONTROL THE MOVEMENT NOT BEING POSSIBLE AND THE PLANE LEFT THE RUNWAY.
- [SDR Y2PA2020090220020](https://openairdocs.org/sdr/Y2PA2020090220020.md): Former · cracked · Aug 27, 2020 · N327US · Doug DC933F · Fuselage Main, Frame
  > DISCREPANCY: DURING C-CHECK AT KDHN FOUND FORWARD SIDE OF FRAME FORMER CRACKED AT FUSELAGE STATION FS 1086 AT LONGERON 28R. CORRECTIVE ACTION: COMMERCIAL JET STOP DRILLED CRACK AND VERIFIED CRACK CONTAINMENT VIA NDT. FABRICATED, DRILLED, DEBURRED, TREATED, P
- [SDR Y2PA2020090220019](https://openairdocs.org/sdr/Y2PA2020090220019.md): Skin · cracked · Aug 27, 2020 · N327US · Doug DC933F · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING C-CHECK AT KDHN, FOUND ON THE UPPER MAIN CARGO DOOR FS313L TO 332L ABOVE WINDOW FRAME, SKIN IS CRACKED ALONG RIVET ROW. CORRECTIVE ACTION: COMMERCIAL JET STOP DRILLED CRACK AND VERIFIED CRACK CONTAINMENT VIA NDT. FABRICATED, DRILLED, DEBUR
- [SDR Y2PA2020090220018](https://openairdocs.org/sdr/Y2PA2020090220018.md): Beam · cracked · Aug 27, 2020 · N327US · Doug DC933F · Fuselage Main, Structure
  > DISCREPANCY: DURING C-CHECK AT KDHN A 0.625 INCH CRACK WAS FOUND ON THE FORWARD ENTRY DOOR #7 BEAM, AFT END OB SIDE. CORRECTIVE ACTION: COMMERCIAL JET STOP DRILLED CRACK AND VERIFIED CRACK CONTAINMENT VIA NDT. FABRICATED, DRILLED, DEBURRED, TREATED, PRIMED AN
- [SDR Y2PA2020090220017](https://openairdocs.org/sdr/Y2PA2020090220017.md): Seat Track · corroded · Aug 27, 2020 · N327US · Doug DC933F · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: DURING C-CHECK AT KDHN CORROSION FOUND AT STATION 639R-658R RBL 0 SEAT TRACK AROUND FASTENERS. CORRECTIVE ACTION: COMMERCIAL JET REMOVED CORRODED SEAT TRACK SECTION AND SPLICED IN SEAT TRACK BETWEEN 588R AND 43.5R RBL 0 IAW DC9 SRM 51-30-1.
- [SDR Y2PA2020090220016](https://openairdocs.org/sdr/Y2PA2020090220016.md): Spar Cap · corroded · Aug 27, 2020 · N327US · Doug DC933F · Wing Spar
  > DURING C-CHECK AT KDHN 3 NDT CONFIRMED CRACKS FOUND ON L/H WING XRS 267 UPPER SPAR CAP DURING ACCOMPLISHMENT OF AD05-07-03, S/B 57-179. REMOVED AND REPLACED DISCREPANT AREA OF THE LT WING UPPER REAR SPAR CAP FROM XRS 167.15 TO XRS 319.5 IAW DC9 S/B 57-179 AND
- [SDR Y2PA2020090220015](https://openairdocs.org/sdr/Y2PA2020090220015.md): Beam · corroded · Aug 27, 2020 · N327US · Doug DC933F · Standard Practices/Structures
  > DISCREPANCY: DURING C-CHECK AT KDHN, CORROSION WAS FOUND ON THE FORWARD CARGO LOWER FUSELAGE BEAM AT STATION 579R – 579L ON THE FORWARD AND AFT ENDS. CORRECTIVE ACTION: COMMERCIAL JET CUT OUT THE DAMAGED SECTION OF THE FLOOR BEAM AT STATION 579 RBL 38.0 TO
- [SDR FXGA20200303001](https://openairdocs.org/sdr/FXGA20200303001.md): Warning Switch · inoperative · Mar 3, 2020 · N935CE · Doug DC933F · Landing Gear Position and Warning
  > LEFT LANDING GEAR DOWN AND LOCK INDICATION INOPERATIVE (BOTH PRIMARY AND SECONDARY SYSTEM INDICATION) ON APPROACH TO BET. AIRCRAFT DIVERTED TO FAI AND MADE ABNORMAL LANDING AFTER VISUAL INSPECTION FROM GROUND THAT GEAR WAS DOWN. INSPECTION OF LMLG INDICATION S
- [SDR FXGA2018102200001](https://openairdocs.org/sdr/FXGA2018102200001.md): Insert · missing · Oct 19, 2018 · N932CE · Doug DC933F · Turbine Engine Accessory Drive
  > ENGINE SHUTDOWN AT 1945 LOSS OF OIL QUANTITY AND OIL TEMP RISING. FOUND TREAD INSERT AND STUD LOST FROM RT ENGINE ACCY DRIVE CASE.
- [SDR FXGA201807051815](https://openairdocs.org/sdr/FXGA201807051815.md): Seat Track · corroded · Jul 5, 2018 · N935CE · Doug DC933F · Fuselage, Seat/Cargo Attach Fittings
  > REPLACEMENT OF SEAT TRACKS AT RBL24 AND RBL9. TO REPLACE CORRODED AND WORN OUT OF LIMITS SEAT TRACKS AT RBL24 BETWEEN S/STA237 AND 609, AND AT RBL9 BETWEEN F/STA 454.5 AND 493.5. REPLACE SEAT TRACK SECTION AT RBL9 BETWEEN EXISTING SPLICES AT F/STA 454.5 AND
- [SDR FXGA2018062700001](https://openairdocs.org/sdr/FXGA2018062700001.md): Downlock Switch · worn · Jun 25, 2018 · N930CE · Doug DC933F · Landing Gear Position and Warning
  > GEAR DOWN FOR LANDING AT PANC, NO GEAR SAFE INDICATION FOR RIGHT MAIN GEAR.
- [SDR K11A2018011691650](https://openairdocs.org/sdr/K11A2018011691650.md): Warning Light · illuminated · Jan 16, 2018 · N916CK · Doug DC933F · Cabin Pressure Control System
  > DESCENDING TO FL 290, THE MASTER WARNING LIGHT ILLUMINATED, SIGNALING A CABIN PRESS ABOVE 10K, USED OXYGEN MASK AND DESCENDED TO FL 240, DECLARED AN EMERGENCY, FOLLOWED REMAINING CHECK LIST PROCEDURE UPON REACH 10000, AND LANDED.
- [SDR K11A2018011591606](https://openairdocs.org/sdr/K11A2018011591606.md): Web · cracked · Jan 15, 2018 · N916CK · Doug DC933F · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR WEBBING CRACKED STA 832 LBL 48. REPAIRED WEBBING AT APPROX STA 832 LBL 48 IAW SRM 53-01 FIG 4 THIS IS A CAT A REPAIR AND NO FURTHER INSPECTION REQUIRED.
- [SDR K11A2018011591605](https://openairdocs.org/sdr/K11A2018011591605.md): Intercostal · cracked · Jan 15, 2018 · N916CK · Doug DC933F · Fuselage Miscellaneous Structure
  > LOWER FWD VHF SUPPORT INTERCOSTAL CRACKED. R&R DAMAGED INTERCOSTAL IAW DWG PL5911412, SRM 51-30-5 PAR 7 PG 12 AND SRM 51-30-2.
- [SDR K11A2018011591604](https://openairdocs.org/sdr/K11A2018011591604.md): Floorbeam · corroded · Jan 15, 2018 · N916CK · Doug DC933F · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR SUPPORT CORROSION AT STA 916 LBL 36, REPAIRED MAIN DECK FLOORBEAM SUPPORT AT STA 916 LBL 36 IAW KA DWG 53301712-1 REV OR. THIS IS A CAT A REPAIR NO FURTHER INSPECTION REQUIRED
- [SDR K11A2018011591603](https://openairdocs.org/sdr/K11A2018011591603.md): Skin · cracked · Jan 15, 2018 · N916CK · Doug DC933F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT STA 1143 ABOUT 3 INCHES ABOVE SKIN LAP ON RT SIDE CRACKED IS ABOUT 1.5 INCHES LONG. REPAIRED CRACK IAW SRM 53-01 FIG 2 PG 12. THIS IS A CAT A REPAIR NO FURTHER INSPECTION REQUIRED
- [SDR K11A2018011591602](https://openairdocs.org/sdr/K11A2018011591602.md): Strap · corroded · Jan 15, 2018 · N916CK · Doug DC933F · Fuselage Miscellaneous Structure
  > CORROSION AT STA 1089 STR 13-16, INSTALLED REPAIR IAW DWG 53301715-1, CAT A REPAIR NO FURTHER INSPECTIONS REQUIRED.
- [SDR K11A2018011591601](https://openairdocs.org/sdr/K11A2018011591601.md): Floorbeam · corroded · Jan 15, 2018 · N916CK · Doug DC933F · Fuselage Main, Floor Beam
  > MAIN DECK FLOORBEAM BS 897, RBL 6 CORRODED. REPAIRED IAW DWG 53301713-1, REV OR.
- [SDR FXGA201711211720](https://openairdocs.org/sdr/FXGA201711211720.md): Fitting · cracked · Nov 21, 2017 · N930CE · Doug DC933F · Fuselage Main, Attach Fittings
  > FITTING AT BS 351 LONGERON 32L CRACKED. REPLACED THE DAMAGED FITTING IAW EA 25-2017-138
- [SDR K11A2017091291603](https://openairdocs.org/sdr/K11A2017091291603.md): Web · cracked · Sep 12, 2017 · N916CK · Doug DC933F · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR WEB UNDER FLOORBOARD FOUND CRACKED
- [SDR K11A2017091291602](https://openairdocs.org/sdr/K11A2017091291602.md): Floor Support · corroded · Sep 12, 2017 · N916CK · Doug DC933F · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT HAS EVIDENCE OF CORROSION AROUND FASTENER.
- [SDR K11A2017091291601](https://openairdocs.org/sdr/K11A2017091291601.md): Floor Support · corroded · Sep 12, 2017 · N916CK · Doug DC933F · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT HAS EVIDENCE OF CORROSION.
- [SDR FXGA201706211713](https://openairdocs.org/sdr/FXGA201706211713.md): Seat Track · corroded · Jun 21, 2017 · N935CE · Doug DC933F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BETWEEN BS 435 AND 511, BL 0. REPLACED THE SEAT TRACK IAW SRM 53-21-0.
- [SDR FXGA20170215001](https://openairdocs.org/sdr/FXGA20170215001.md): Position Switch · sticking · Feb 11, 2017 · N930CE · Doug DC933F · Landing Gear Door Retract Section
  > DURING GEAR RETRACTION, GEAR DOOR OPEN LIGHT AND GEAR RED UNSAFE LIGHTS FOR LEFT AND RIGHT MAIN GEAR ILLUMINATED WITH GEAR HANDLE IN UP POSITION.
- [SDR FXGA201701121701](https://openairdocs.org/sdr/FXGA201701121701.md): Skin · cracked · Jan 12, 2017 · N932CE · Doug DC933F · Fuselage Main, Plate/Skin
  > SKIN CRACK AT RIGHT HAND FUSELAGE STATION 1143 STRINGER RIGHT 14. MAJOR REPAIR OF CRACK PER SRM REFERENCE. REPAIR PER SRM 53-01 FIGURE 2 (SHEET 3).
- [SDR FXGA201612301644](https://openairdocs.org/sdr/FXGA201612301644.md): Skin · cracked · Dec 30, 2016 · N935CE · Doug DC933F · Fuselage Main, Plate/Skin
  > SKIN CRACK AT RIGHT HAND STA 1144 STRINGER R15. MAJOR REPAIR OF CRACK PER SRM REFERENCE. REPAIR PER SRM 53-01 FIGURE 2 (SHEET 3).
- [SDR FXGA201612301642](https://openairdocs.org/sdr/FXGA201612301642.md): Skin · cracked · Dec 30, 2016 · N935CE · Doug DC933F · Fuselage Main, Plate/Skin
  > SKIN CRACK AT LEFT HAND STA 1132 STRINGER L14. MAJOR REPAIR OF CRACK PER SRM REFERENCE. REPAIR PER SRM 53-01 FIGURE 2 (SHEET 3).
- [SDR K11A2016110416001](https://openairdocs.org/sdr/K11A2016110416001.md): Bulkhead Web · corroded · Nov 4, 2016 · N916CK · Doug DC933F · Fuselage Main, Bulkhead
  > LEFT WHEEL WELL HAS CORROSION, UPPER PRESSURE BULKHEAD.
- [SDR FXGA201610261638](https://openairdocs.org/sdr/FXGA201610261638.md): Skin · cracked · Oct 26, 2016 · N930CE · Doug DC933F · Fuselage Main, Plate/Skin
  > REPAIR OF CRACKS IN FUSELAGE SKIN FS 102.5 BELOW STRINGER R18. REPAIR CRACKS EXTENDING FROM RIVETS IN SKIN AT FS 102.5 STRUCTURAL REPAIR MANUAL 53-01 FIGURE 4 (SHEET 4).
- [SDR FXGA201610261637](https://openairdocs.org/sdr/FXGA201610261637.md): Structure · cracked · Oct 25, 2016 · N930CE · Doug DC933F · Fuselage Miscellaneous Structure
  > REPAIR OF 4" CRACK IN FUSELAGE TAIL STA 1205 RT 3 O-CLOCK POSITION. MAJOR REPAIR OF CRACK PER SRM REFERENCE SRM 53-01 FIGURE 4.
- [SDR FXGA201610240001](https://openairdocs.org/sdr/FXGA201610240001.md): Support Bracket · cracked · Oct 24, 2016 · N930CE · Doug DC933F · Trailing Edge Flap Actuator
  > RIGHT FLAP I/B ACTUATOR SUPPORT BRACKET CRACKED.
- [SDR K11A2016110416005](https://openairdocs.org/sdr/K11A2016110416005.md): Skin · corroded · Oct 13, 2016 · N916CK · Doug DC933F · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN FWD LOWER CARGO DOOR CUTOUT CORROSION, LONGERON 25
- [SDR K11A2016110416006](https://openairdocs.org/sdr/K11A2016110416006.md): Pan · corroded · Oct 1, 2016 · N916CK · Doug DC933F · Fuselage Miscellaneous Structure
  > LEFT MLG WW UPPER RETAINER PAN CORRODED.
- [SDR K11A2016110416004](https://openairdocs.org/sdr/K11A2016110416004.md): Longeron · corroded · Sep 28, 2016 · N916CK · Doug DC933F · Fuselage Main, Longeron/Stringer
  > LONGERON CORRODED.
- [SDR K11A2016110700002](https://openairdocs.org/sdr/K11A2016110700002.md): Skin · corroded · Sep 26, 2016 · N916CK · Doug DC933F · Trailing Edge Flaps
  > LEFT WING FLAP LOWER SKIN CORRODED, XFLS 326.
- [SDR K11A20161416001](https://openairdocs.org/sdr/K11A20161416001.md): Skin · cracked · Sep 26, 2016 · N916CK · Doug DC933F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BS 266 LONGERON 5L HAS EVIDENCE OF A CRACK
- [SDR K11A2016110416008](https://openairdocs.org/sdr/K11A2016110416008.md): Skin · cracked · Sep 22, 2016 · N916CK · Doug DC933F · Aerodynamic Fairings
  > TAILCONE EXTERNAL SKIN RT SIDE CRACKED.
- [SDR K11A2016110416003](https://openairdocs.org/sdr/K11A2016110416003.md): Floor Support · corroded · Sep 22, 2016 · N916CK · Doug DC933F · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT BRACKET CORRODED.
- [SDR K11A2016110416007](https://openairdocs.org/sdr/K11A2016110416007.md): Skin · cracked · Sep 16, 2016 · N916CK · Doug DC933F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED.
- [SDR K11A2016080391601](https://openairdocs.org/sdr/K11A2016080391601.md): Warning Light · illuminated · Aug 1, 2016 · N916CK · Doug DC933F · Engine Oil Indicating System
  > PERFORMED PRECAUTIONARY SHUTDOWN OF LEFT ENGINE DUE TO OIL PRESSURE LOW LIGHT, LOW OIL PRESSURE & ZERO ON OIL QUANTITY
- [SDR K11A2016110291508](https://openairdocs.org/sdr/K11A2016110291508.md): Floorboard · corroded · Jun 20, 2016 · N916CK · Doug DC933F · Fuselage Floor Panel
  > AFT OF R1 DOOR FLOORBOARD CORROSION.
- [SDR K11A2016062616001](https://openairdocs.org/sdr/K11A2016062616001.md): Fuel Tank · corroded · Jun 20, 2016 · N916CK · Doug DC933F · Fuel Storage
  > CORROSION ON THE FORWARD SIDE OF THE FUEL TANK AT STA 598, RBL 34.
- [SDR FXGA201606131612](https://openairdocs.org/sdr/FXGA201606131612.md): Cusp Web · damaged · Jun 13, 2016 · N935CE · Doug DC933F · Fuselage Miscellaneous Structure
  > MAIN DECK CUSP WEBS DAMAGED, STA 322-455, RBL 54. DURING THE INSPECTION, DAMAGE WAS DISCOVERED IN VARIOUS AREA OF THE OTBD CUSP WEB BETWEEN FS 322-455. REMOVE EXISTING RING DOUBLERS IN AREAS OF PANEL TO BE TRIMMED OR REPLACED AND REPAIR IAW 53-006-R1 AND R2.
- [SDR FXGA201606141611](https://openairdocs.org/sdr/FXGA201606141611.md): Bulkhead · cracked · Jun 13, 2016 · N935CE · Doug DC933F · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AT LBL 40, FRAME STA 996 LT. DURING INSPECTION A CRACK WAS DISCOVERED. AFT PRESSURE BULKHEAD CRACKED AT LBL 40, FRAME STA 996 LT. REMOVE CLIP FROM RADIAL TRIM OUT DAMAGE HAT SECTION. FABRICATED REPAIR ANGLES AND INSTALLED IAW
- [SDR FXGA201606101610](https://openairdocs.org/sdr/FXGA201606101610.md): Pan · corroded · Jun 10, 2016 · N935CE · Doug DC933F · Cargo/Baggage Doors
  > AFT CARGO PIT DOOR INTERNAL PAN CORROSION REPAIR. AFT CARGO PIT DOOR INTERNAL PAN HAS NUMEROUS AREAS OF CORROSION AT BLIND HI-SHEAR LOCATIONS. REMOVE ALL EVIDENCE OF CORROSION FOR CARGO DOOR PAN. FABRICATE DOUBLERS 063 2024 T3, AND INSTALL IAW DOCUMENT N935CE
- [SDR FXGA201606101609](https://openairdocs.org/sdr/FXGA201606101609.md): Skin · damaged · Jun 10, 2016 · N935CE · Doug DC933F · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STABILIZER L/E DAMAGED AT BS XFS 229-235, 4" DAMAGE TRIMOUT. MAKE CUTOUT IAW SRM 55-03, FIG 2, SHT 3, DEVIATIONS APPROVED IAW DOCUMENT N935CE-055-002, CREATE DOUBLER & FILLER.
- [SDR FXGA201606011606](https://openairdocs.org/sdr/FXGA201606011606.md): Window Frame · corroded · Jun 6, 2016 · N935CE · Doug DC933F · Fuselage Main, Structure
  > REPLACEMENT OF PILOT TO CENTER WINDOW LOWER "Z" FRAME. PILOT`S WINDOW TO CENTER WINDOW LOWER "Z" FRAME HAS CORROSION, SHEARED RIVET. THE REPAIR ITSELF INVOLVED THE 2 STAINLESS ANGLES, PN 5910075-99/-100, AT THE LOWER COCKPIT WINDOWS, LT AND RT SIDE. THE CORR
- [SDR K11A2016032291601](https://openairdocs.org/sdr/K11A2016032291601.md): Battery · damaged · Mar 22, 2016 · N916CK · Doug DC933F · Battery/Charger System
  > WITH AIRCRAFT ON GROUND, ATTEMPTED TO START APU TO REPOSITION, FOUND SHIP BATTERIES WEAK, INVESTIGATED AND DISCOVERED ONE OF THE SHIP BATTERY CASES DAMAGED. REPLACED BATTERIES AND CHARGER.

Next page: https://openairdocs.org/model/douglas-dc-9-33f/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 = 'DC933F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-9-33f/reports

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