# Service difficulty reports: N935CE

A list on [N935CE](https://openairdocs.org/aircraft/N935CE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [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 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 FXGA201931011913](https://openairdocs.org/sdr/FXGA201931011913.md): Floorbeam · corroded · Jan 31, 2019 · N935CE · Doug DC9 · Fuselage Main, Floor Beam
  > FLOORBEAM STA 756, RBL 30 UPPER SURFACE CORROSION BLENDOUT. DRILL START DAMAGE TO MAIN CARGO DOOR FWD FRAME BEYOND SRM LIMITS. THE BLEND IS ADJACENT TO FASTENER THAT WAS NOTED TO BE A NAS1097AD6 RIVET BY THE CUSTOMER AND HAS A 0.400" EDGE MARGIN. THE TEE IS
- [SDR FXGA201931011901](https://openairdocs.org/sdr/FXGA201931011901.md): Skin · corroded · Jan 31, 2019 · N935CE · Doug DC9 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN JUST AFT OF STA 756 AT LONGERON 29R EXFOLIATION CORROSION REPAIR. FUSELAGE SKIN JUST AFT OF STA 756 AT LONGERON 29R WAS FOUND TO HAVE EXFOLIATION CORROSION. REPAIR FUSELAGE SKIN JUST AFT OF STA 756 AT LONGERON 29R.
- [SDR FXGA2019031200000](https://openairdocs.org/sdr/FXGA2019031200000.md): Unknown · malfunctioned · Nov 10, 2018 · N935CE · Doug DC9 · Cabin Pressure Control System
  > LOSS OF PRESSURIZATION @ FL250 RIGHT PACK WAS DMI. FOLLOWED QRH EMERGENCY CHECK LIST INSTRUCTIONS TO 10,000 FEET. DESCENDED PER QRH TO 10,000 FEET.
- [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 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 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 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 FXGA201509221537](https://openairdocs.org/sdr/FXGA201509221537.md): Seat Track · damaged · Sep 29, 2015 · N935CE · Doug DC933F · Fuselage, Seat/Cargo Attach Fittings
  > DAMAGED SEAT TRACK LUG AT FS 400, LBL 54. TO REMOVE AN OUT OF LIMIT IAW SRM CHAPTER 53-05 FIGURE 4B SHEET 1, SEAT TRACK LUG TO PRECLUDE THE INSTALLATION OF ANCHORING DEVICES IN THE DAMAGED AREA. TRIM OUT DAMAGED & MATCHING LUGS IAW DWG 1537-01. TRIM FLUSH T
- [SDR FXGA20141224001](https://openairdocs.org/sdr/FXGA20141224001.md): Unknown · malfunctioned · Dec 23, 2014 · N935CE · Doug DC933F · Engine (Turbine/Turboprop)
  > AT APPROX 2245Z & CLIMBING THROUGH FL280, R OIL STRAINER CLOGGING, ANNUNCIATOR ILLUMINATED. PERFORMED ABNORMAL CHECKLIST. REDUCED POWER TO IDLE ON RT ENG. DECLARED AN EMER & RETURNED.
- [SDR FXGA201409241439](https://openairdocs.org/sdr/FXGA201409241439.md): Seat Track · corroded · Sep 24, 2014 · N935CE · Doug DC933F · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON INBD LT SEAT TRACK IN FLIGHT DECK. AFTER CORROSION REMOVAL, FOUND SEAT TRACK TO BE OUT OF LIMITS. REMOVED & FABRICATED NEW SECTION OF TRACK & INSTALLED IAW DC9-SRM 51-40-4, 51-30-2 & 53-05 FIG 92.
- [SDR 7AHR201409242160](https://openairdocs.org/sdr/7AHR201409242160.md): Finger Doubler · corroded · Sep 23, 2014 · N935CE · Doug DC933F · Fuselage Main, Structure
  > LONGERON 26 RIGHT BS 598 INTERNAL FINGER DOUBLER PILLOWING AND CRACKED AT SPLICE FITTING. AFTER CORROSION REMOVAL THE AREA WAS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 51-10-3, 53-04-1, 51-30-5 AND 51-04-03.
- [SDR 7AHR201409242362](https://openairdocs.org/sdr/7AHR201409242362.md): Seat Track · corroded · Sep 23, 2014 · N935CE · Doug DC933F · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION WAS NOTED IN THE COCKPIT LT INBD SEAT TRACK. REMOVED CORROSION AND FOUND IT TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IAW SRM 51-10-3, 51-10-04, 51-30-2 AND 53-05, FIG 92.
- [SDR FXGA201409231438](https://openairdocs.org/sdr/FXGA201409231438.md): Skin · gouged · Sep 23, 2014 · N935CE · Doug DC933F · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER LT TIP PLATING REPAIR FROM ZV73 TO ZV147 BETWEEN YV157 & YV172. GOUGES FOUND ON FWD LT SIDE OF VERTICAL STABILIZER UNDER UPPER & LOWER BANANA FAIRING.
- [SDR FXGA201409231437](https://openairdocs.org/sdr/FXGA201409231437.md): Web · dented · Sep 23, 2014 · N935CE · Doug DC933F · Fuselage Miscellaneous Structure
  > NOSE LANDING GEAR SUPPORT WEB RT SIDE REPAIR. REPAIRS WEB DENTED IN RT SIDE NOSE GEAR WW NEAR RT TRUNNION FITTING.
- [SDR FXGA201409231436](https://openairdocs.org/sdr/FXGA201409231436.md): Finger Doubler · corroded · Sep 23, 2014 · N935CE · Doug DC933F · Fuselage Main, Plate/Skin
  > REPAIR AT LONGERON 26RT FS 598 INTERNAL FINGER DOUBLER. LONGERON 26RT FS 598 INTERNAL FINGER DOUBLER IS PILLOWING & CRACKED AT SLICE FITTING LOCATION. REPAIR THE DOUBLER IAW SRM.
- [SDR 7AHR2014092300002](https://openairdocs.org/sdr/7AHR2014092300002.md): Structure · gouged · Sep 22, 2014 · N935CE · Doug DC933F · Vertical Stabilizer
  > GOUGED AREAS WERE FOUND ON FWD LT SIDE OF VERTICAL STABILIZER UNDER UPPER AND LOWER BANANA FAIRING. GOUGED AREAS WERE FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR TO TIP PLATING IAW FLIGHT VEHICLE CONSULTING DWG NR 55-14233-1, REV-NEW, DATED SE
- [SDR 7AHR201409232049](https://openairdocs.org/sdr/7AHR201409232049.md): Web · dented · Sep 22, 2014 · N935CE · Doug DC933F · Fuselage Main, Structure
  > WEB DENTED IN RT SIDE NOSE GEAR WHEEL WELL NEAR RT TRUNION FITTING. REMOVED DAMAGE FROM WEB, FABRICATED REPAIR PARTS FOR DOUBLER AND INSTALLED IAW FLIGHT VEHICLE CONSULTING, DWG 53-14230-1, REV NEW, DATED SEPT 4, 2014. APPROVAL FOR REPAIR IAW FORM 8110-3.
- [SDR FXGA20131121001](https://openairdocs.org/sdr/FXGA20131121001.md): Unknown · malfunctioned · Nov 20, 2013 · N935CE · Doug DC933F · Cabin Pressure Control System
  > AT ALTITUDE 350 CABIN PRESS LIGHT ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES, COULD NOT RESTORE PRESS. DECLARED AN EMERGENCY WITH CTR AT 0253Z. DESCENDED TO 10,000 CONTINUED TO FAI.

## 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 = 'N935CE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N935CE/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.