# Service difficulty reports: N933DL, cancelled Sep 16, 2019

A list on [N933DL, cancelled Sep 16, 2019](https://openairdocs.org/deregistered/N933DL-2019-09-16.md).

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

Page 1 of 4 · 166 reports

- [SDR DALA2018090305398](https://openairdocs.org/sdr/DALA2018090305398.md): Smoke Detector · defective · Aug 31, 2018 · N933DL · Doug MD88 · Smoke Detection
  > CABIN CLEANING CREW REPORTS AFT LT LAV SMOKE DETECTOR CHIRPING. REPLACED AFT LEFT DETECTOR PER AMM26-13. TESTS NORMAL.
- [SDR DALA2018081004974](https://openairdocs.org/sdr/DALA2018081004974.md): Smoke Detector · false activation · Aug 9, 2018 · N933DL · Doug MD88 · Smoke Detection
  > AFT LAVATORY SMOKE DETECTOR ACTIVATED ON THE GROUND WHILE BOARDING. REPLACED THE SMOKE DETECTOR IAW AMM 26-13-00. OK FOR SERVICE.
- [SDR DALA2018061103935](https://openairdocs.org/sdr/DALA2018061103935.md): Structure · dented · Jun 11, 2018 · N933DL · Doug MD88 · Nacelle/Pylon, Main Frame
  > DURING A PREFLIGHT, FOUND SIGNIFICANT NOSE COWL DENTS AT 11:45 POSITION. REMOVED THE 1 ENGINE INLET COWL IAW PPBM 71-00 AND ERA 569353-14 AND INSTALLED SERVICEABLE INLET NOSE COWL.
- [SDR DALA2018030801470](https://openairdocs.org/sdr/DALA2018030801470.md): Sensor · out of tolerance · Mar 6, 2018 · N933DL · Doug MD88 · Landing Gear Position and Warning
  > ON CLIMB OUT RED NOSE GEAR UNSAFE LIGHT CAME ON AND BACK OFF SEVERAL TIMES IN LIGHT/MED TURB. LONGEST TIME ON APPROX 1 MIN. NEVER GOT GEAR DOOR OPEN LIGHT. GOT QRH OUT 1 LIGHT WENT OUT AND DID NOT COME BACK ON. NOTIFIED MAINT. PERFORMED NO GO ODI PREVENTION OF
- [SDR DALA2018030801469](https://openairdocs.org/sdr/DALA2018030801469.md): Wire · unsecure · Mar 6, 2018 · N933DL · Doug MD88 · Light System Wiring
  > CABIN SERVICE REPORTED WIRES LOOSE AT SEAT 27DE. FOUND WIRES PULLED FROM EMERGENCY LIGHTS SEAT PLUG. RESECURED SAME AND SECURED WIRING. LIGHTS OP NORMALLY.
- [SDR DALA2018021700967](https://openairdocs.org/sdr/DALA2018021700967.md): Service Door · cracked · Feb 17, 2018 · N933DL · Doug MD88 · Fluid Service Doors
  > AFT LAV SERVICE DOOR CRACK IN FUSELAGE. TRACKING FOR ACCOMPLISHMENT OF SECTION III: PERMANENT REPAIR PER ER/A 538941-14 REV B. FUSELAGE SKIN BELOW AFT LAVATIRY SERVICE PANEL WAS PERMANENT REPAIRED PER ER/A 538941-14 REV.C AND ETI 88-18-008 REV.2. (LP0226265)
- [SDR DALA2018021700966](https://openairdocs.org/sdr/DALA2018021700966.md): Vane · delaminated · Feb 16, 2018 · N933DL · Doug MD88 · Trailing Edge Flaps
  > DELAMINATED OTBD GUIDE VANE OF INBD FLAP ON THE LT WING. THE GUIDE VANE WAS REMOVED AND REPLACED IAW AMM 27-51-03-201.
- [SDR DALA2018021700965](https://openairdocs.org/sdr/DALA2018021700965.md): Bulkhead · cracked · Feb 16, 2018 · N933DL · Doug MD88 · Fuselage Main, Bulkhead
  > CRACKS FOUND ON THE AFT CARGO BAY FWD PRESSURE BULKHEAD BS 1003, Z-6 TO Z-9, LBL 26 TO 26. THE PRESSURE BULKHEAD WAS REPAIRED IAW ER/A 565886-14, REV ORIGINAL.
- [SDR DALA2018021600934](https://openairdocs.org/sdr/DALA2018021600934.md): Hose · torn · Feb 15, 2018 · N933DL · Doug MD88 · Passenger Oxygen System
  > DURING INSPECTION OF LAVATORY OXYGEN MASK, HOSE ON RT AFT LAVATORY WAS FOUND TORN. IN REF 3500-7457 STEP 5. LAVATORY OXYGEN MASK HOSE ON RT AFT LAVATORY WAS REPLACED PER AMM 35-22-02.
- [SDR DALA2018021600933](https://openairdocs.org/sdr/DALA2018021600933.md): Skin · cracked · Feb 15, 2018 · N933DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED SKIN BTW BEAM NR 4 TO 5 MID SECTION AT MAIN ENTRANCE DOOR. CRACKED SKIN BTW BEAM NR 4 TO 5 MID SECTION WAS REPAIRED PER ER/A:501106-14MA REVISION: C READY FOR ENTRY PERFORM VISUAL DEACL INSPECTION CONDITION EVERY C (L1).
- [SDR DALA2018021500931](https://openairdocs.org/sdr/DALA2018021500931.md): Tape · missing · Feb 14, 2018 · N933DL · Doug MD88 · Hydraulic Pump, Auxiliary
  > AWR AD INITIAL INSPECTION, MISSING AND WORN TIE TAPE ON AUX HYDRAULIC PUMP POWER FEEDER WIRING. TIE TAPE WAS REPLACED PER ERA 467688-14MAAD REV D.
- [SDR DALA2018021500901](https://openairdocs.org/sdr/DALA2018021500901.md): Skin · cracked · Feb 14, 2018 · N933DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FOUND A CRACK IN THE FUSELAGE BELOW THE AFT LAVATORY SERVICE DOOR. THE SKIN WAS REPAIRED IAW ER/538941-14, REV C, AND ETI-88-18.
- [SDR DALA2018021500900](https://openairdocs.org/sdr/DALA2018021500900.md): Frame · cracked · Feb 14, 2018 · N933DL · Doug MD88 · Fuselage Main, Frame
  > FOUND A CRACKED FRAME BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-2 AND 53-14-4, FIG 3.
- [SDR DALA2018021400876](https://openairdocs.org/sdr/DALA2018021400876.md): Pin · missing · Feb 13, 2018 · N933DL · Doug MD88 · Escape Slide
  > MISSING SECURITY PIN ON AFT PASSENGER ENTRANCE EVACUATION SLIDE AND TAIL CONE EVACUATION SLIDE IN REF 2520-2169. PIN ON TAIL CONE EVACUATION SLIDE AND PIN ON AFT PASSENGER ENTRANCE EVACUATION SLID WERE INSTALLED PER AMM 25-62-00-201.
- [SDR DALA2018021400875](https://openairdocs.org/sdr/DALA2018021400875.md): Longeron · corroded · Feb 13, 2018 · N933DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AWR HIDDEN CORROSION: CORROSION WAS FOUND ON LONGERON 22L FROM STA Y=1331 TO Y=1333 IN AFT CARGO COMPARTMENT DURING REPAIR OF AFT LAVATORY SERVICE PANEL REF NRC S/N 00051. LEVEL CORROSION 2 DAMAGE LONGERON WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-02 FIG 18.
- [SDR DALA2018021300856](https://openairdocs.org/sdr/DALA2018021300856.md): Pan · cracked · Feb 12, 2018 · N933DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED PAN ABOVE THE NR 1 BEAM, FWD EDGE AT MAIN ENTRANCE DOOR. THE PAN WAS REPAIRED IAW SRM 52-05, PAR 14, FIG 18A.
- [SDR DALA2018021200828](https://openairdocs.org/sdr/DALA2018021200828.md): Guide Vane · worn · Feb 11, 2018 · N933DL · Doug MD88 · Trailing Edge Flaps
  > WEAR ON LT WING OUTBOARD FLAP INBOARD GUIDE VANE STA XFLS=151. LT WING OUTBOARD FLAP INBOARD GUIDE VANE STA XFLS=151 WAS REPAIRED PER SRM 57-03 D PARAGRAPH 11 AND 2000-8149-01.
- [SDR DALA2018021100816](https://openairdocs.org/sdr/DALA2018021100816.md): Skin · cracked · Feb 10, 2018 · N933DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > CRACK ON VERT STAB SKIN LT SIDE NEAR FRONT SPAR STA ZFS=17. CRACKS ON VERT STAB SKIN LT SIDE NEAR FRONT SPAR STA ZFS=17.6 WERE REPAIRED PER SRM 51-30-8 SRM 55-01 FIG 2 (SHEET 2) AND SRM 51-60-0 PAR 5(O). PERFORM VISUAL INSPECTION, FREQUENCY NOT EXCEEDING C-CHE
- [SDR DALA2017122208801](https://openairdocs.org/sdr/DALA2017122208801.md): Structure · cracked · Dec 20, 2017 · N933DL · Doug MD88 · Cargo/Baggage Doors
  > WHILE C/W PACK CONFIDENCE CHECK, FOUND A LARGE LEAK AT THE TOP OF AFT BAG BIN DOOR. 6 IN CRACK IN TOP OF BAG BIN DOOR. DOOR WAS REPLACED IAW AMM 52-31.
- [SDR DALA2017061204653](https://openairdocs.org/sdr/DALA2017061204653.md): Ballast · miswired · Jun 11, 2017 · N933DL · Doug MD88 · Passenger Compartment Lighting
  > AFT STAIRWAY FLUORESCENT LIGHT FOUND INOPERATIVE. FOUND THE BALLAST MISWIRED. CONNECTED LEFT BALLAST IAW WDM 33-23-01. OPS CHECKED OK.
- [SDR DALA2016112509295](https://openairdocs.org/sdr/DALA2016112509295.md): Light · sparks · Nov 24, 2016 · N933DL · Doug MD88 · Flight Compartment Lighting
  > FIRST OFFICER`S FLIGHT KIT LIGHT SPARKED IN FLIGHT. R & R THE LIGHT IAW AMM 33-10-00 OPS CHECKED OK.
- [SDR DALA2016072505545](https://openairdocs.org/sdr/DALA2016072505545.md): Wire Harness · damaged · Jul 23, 2016 · N933DL · Doug MD88 · Light System Wiring
  > ROW 20ED EMERGENCY SEAT LIGHT INOPERATIVE. REMOVED & REPLACED UNDERSEAT HARNESS. OPS CHECK GOOD.
- [SDR DALA2016071805387](https://openairdocs.org/sdr/DALA2016071805387.md): Acm · contaminated · Jul 17, 2016 · N933DL · Doug MD88 · Cabin Cooling System
  > ACFT DIVERTED DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND LIGHT OIL FILM ON EXIT OF RIGHT ACM. REPLACED RIGHT ACM PER AMM. COMPLIED WITH DUCT BURNOUT, NO SMOKE OR ODOR NOTED. THE AIRCRAFT RETURNED TO SERVICE.
- [SDR DALA2016071805386](https://openairdocs.org/sdr/DALA2016071805386.md): Oil Cap · detached · Jul 16, 2016 · N933DL · Doug MD88 · APU Oil System
  > RETURNED DUE TO SMOKE IN THE AFT CABIN. MAINTENANCE FOUND APU INLET CONTAMINATED WITH OIL. MAINTENANCE FOUND OIL CAP OFF. CLEANED APU INLET AND DUCTS AND COMPLIED WITH DUCT BURNOUT. AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR DALA2016050903832](https://openairdocs.org/sdr/DALA2016050903832.md): Hydraulic System · contaminated · May 8, 2016 · N933DL · Doug MD88 · Hydraulic System, Main
  > ENROUTE RT HYDRAULIC PRESSURE LOW AND RUDDER CONTROL MAN. RT HYD PRESSURE "0", HYD QTY INITIALLY WENT TO 3 QTS THEN TO 19 QTS. FOLLOWED QRH PROCEDURE NORMAL LANDING AND CONFIGURATION. FOUND BOTH HYD SYS REQUIRED BLEED DUE TO AIR IN SYS. REPLACED RT HYD FIL
- [SDR DALA2016042503299](https://openairdocs.org/sdr/DALA2016042503299.md): Battery Pack · inoperative · Apr 23, 2016 · N933DL · Doug MD88 · Light System Wiring
  > MAINTENANCE FOUND THE OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROWS 11 AND 15. THE BATTERY PACK BATTERIES WERE REPLACED. THE LIGHTS CHECKED OK.
- [SDR DALA2016020500899](https://openairdocs.org/sdr/DALA2016020500899.md): Rudder Pedal · binding · Feb 4, 2016 · N933DL · Doug MD88 · Rudder Control System
  > CAPT RUDDER PEDALS BIND AT HALF TRAVEL. FOUND CABLE ATTACH BOLT COTTER PIN EATCHING ON PLASTIC SESRIS COVER REMOVED BOLT. OK TO INSTALL. CAPT RUDDER PEDAL CABLE 2A BOLT INSTALLED BOLT IAW AMM 27-20. OPS CHECK GOOD.
- [SDR DALA2016111608843](https://openairdocs.org/sdr/DALA2016111608843.md): Access Door · cracked · Jan 29, 2016 · N933DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK AND CORROSION ON POTABLE WATER SERVICE ACCESS DOOR. CRACK AND CORROSION WERE ATTENDED WITH ER/A.
- [SDR DALA2016013000754](https://openairdocs.org/sdr/DALA2016013000754.md): Skin · cracked · Jan 29, 2016 · N933DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACKED PREVIOUS REPAIR DOUBLER ON INNER FUSELAGE SKIN BETWEEN LONGERONS 2L-2R NEXT TO BS 1463. DAMAGE AREA WAS REPAIRED IAW ER/A 541633-14, REV ORIGINAL.
- [SDR DALA2016013000752](https://openairdocs.org/sdr/DALA2016013000752.md): Skin · damaged · Jan 29, 2016 · N933DL · Doug MD88 · Fuselage Main, Plate/Skin
  > ELONGATED FASTENERS HOLE ON FUSELAGE SKIN AT BELLY DRAIN ATTACHMENT POINT BS 295-296 BETWEEN LONGERON 30 AND 29 LT C1 CARGO. DAMAGE WAS CUT OUT REPAIR PARTS WERE FABRICATED, TREATED AND PAINTED REPAIR PARTS WERE INSTALLED IAW SRM 53-04-2, FIG 2, 51-10-3 PAR
- [SDR DALA2016012900714](https://openairdocs.org/sdr/DALA2016012900714.md): Skin · cracked · Jan 28, 2016 · N933DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN BS 1309 BETWEEN LONGERONS 6 - 7L. REPAIRED IAW ETI-88-16-035 R2 AND ER/A 541634-14, REV. ORIGINAL.
- [SDR DALA2016012900711](https://openairdocs.org/sdr/DALA2016012900711.md): Angle · cracked · Jan 27, 2016 · N933DL · Doug MD88 · Vertical Stabilizer
  > CRACKED INNER ANGLE ON DORSAL FIN, REF BS 1427 BETWEEN LONGERONS 1 AND 2 RT. ANGLES WERE REPLACED IAW DWG 5912188 AND SRM 51-30-5.
- [SDR DALA2016012800708](https://openairdocs.org/sdr/DALA2016012800708.md): Web · cracked · Jan 27, 2016 · N933DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED MEMBRANE OF BS 1485 AFT FACE AND 2HRS POSITION. CRACK WAS STOPPED AND REPAIRED ON MEMBRANE IAW SRM 51-01, PAR 21 AND SRM 53-01, FIG 2.
- [SDR DALA2016012800707](https://openairdocs.org/sdr/DALA2016012800707.md): Vane · worn · Jan 27, 2016 · N933DL · Doug MD88 · Trailing Edge Flaps
  > WEAR ON PREVIOUS REPAIR DOUBLER ON MID FLAP VANE GUIDE AT RT WING OTBD FLAP. MID FLAP VANE GUIDE AT RT WING OTBD FLAP WAS REPAIRED IAW SRM 57-03D, PAR 11.
- [SDR DALA2016012500573](https://openairdocs.org/sdr/DALA2016012500573.md): Longeron · cracked · Jan 24, 2016 · N933DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 4LT BS 160 AT CPAX. CEILING PANEL AT LONGERON 4 LT 160 WAS REMOVED IAW AMM 20-30-01-201, FASTENERS WERE REMOVED IAW SRM 51-30-5, HFEC INSPECTION ACCOMPLISHED IAW DC/MD NDTSPM 06-10-01- 001. NO CRACKS WERE FOUND CEILING PANEL, WAS RE-INSTALL
- [SDR DALA2016012500559](https://openairdocs.org/sdr/DALA2016012500559.md): Skin · damaged · Jan 24, 2016 · N933DL · Doug MD88 · Fuselage Main, Plate/Skin
  > SCRATCH ON RT WINDOW BELT BETWEEN BS 1155 - 1174 UPPER SURFACE. SCRATCHES WERE BLEND OUT FOUND WITHIN LIMITS IAW SRM 53-05, FIG 111 AND ER/A 543131.14, REV ORIGINAL. AREAS WERE TREATED IAW SRM 51-10-03, PAR 21.
- [SDR DALA2016012500556](https://openairdocs.org/sdr/DALA2016012500556.md): Doubler · cracked · Jan 24, 2016 · N933DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED AFTER PAN REPAIR DOUBLER BETWEEN FRI 5/6 AT ROLLER TRACK AREA OF FWD ENTRY DOOR. DOUBLER WAS REPLACED IAW SRM 51-30-2, 51-30-1, 51-30-4, 51-10-2, 51-10-3 PAR 14 AND 21 AND DWG 5914121, REV AV.
- [SDR DALA2016012500555](https://openairdocs.org/sdr/DALA2016012500555.md): Frame · cracked · Jan 24, 2016 · N933DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED FRAME NR 8 ON AFTER EDGE AREA OF FWD ENTRY DOOR. FRAME NR 8 OF FWD ENTRY DOOR WAS REPAIRED IAW SRM 52-05D, FIG 111.
- [SDR DALA2016012500564](https://openairdocs.org/sdr/DALA2016012500564.md): Intercostal · cracked · Jan 22, 2016 · N933DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED INTERCOSTAL BETWEEN FRAME 4/5 ON COVER HANDLE ATTACHMENT AREA OF FWD ENTRY DOOR. INSTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-10-3 PAR 14/21 AND 51-10-4.
- [SDR DALA2016012200532](https://openairdocs.org/sdr/DALA2016012200532.md): Access Panel · damaged · Jan 20, 2016 · N933DL · Doug MD88 · Wing, Plate/Skin
  > DAMAGE FUEL SECOND ACCESS PLATE 1307C. FUEL SECOND ACCESS PLATE WAS REPLACED.
- [SDR DALA2016082910214](https://openairdocs.org/sdr/DALA2016082910214.md): Skin · cracked · Aug 30, 2015 · N933DL · Doug MD88 · Fuselage Main, Plate/Skin
  > ER/A 538941-14 SECTION 1 ACCOMPLISHED AND CLASSIFIED AS A MAJOR REPAIR. CRACK IN THE FUSELAGE SKIN NEAR THE AFT LAV SERVICE DOOR CUTOUT.
- [SDR DALA2015083105328](https://openairdocs.org/sdr/DALA2015083105328.md): Skin · cracked · Aug 28, 2015 · N933DL · Doug MD88 · Fuselage Main, Plate/Skin
  > PRIOR TO PUSH BACK, GROUND CREW FOUND A CRACK AROUND THE AFT LAV SERVICE RECEPTICLE SKIN. COMPLIED WITH ERA 538941-14, REV "ORIGINAL.
- [SDR DALA2015061103696](https://openairdocs.org/sdr/DALA2015061103696.md): Wire · pulled · Jun 9, 2015 · N933DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 26D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND WIRES PULLED OUT OF THE LIGHT SOCKET. THE LIGHT ASSEMBLY WAS REPLACED AND THE SYSTEM RETURNED TO NORMAL OPERATION.
- [SDR DALA2015011500357](https://openairdocs.org/sdr/DALA2015011500357.md): Lanyard · damaged · Jan 14, 2015 · N933DL · Doug MD88 · Escape Slide
  > DURING EMERGENCY EQUIPMENT CHECK FOUND PAX DOOR SLIDE LANYARD FRAYED AND DAMAGED. REPLACED LANYARD IAW AMM 25-62-00.
- [SDR DALA2014112006197](https://openairdocs.org/sdr/DALA2014112006197.md): Connector · damaged · Nov 19, 2014 · N933DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 24DE WAS INOPERATIVE. FOUND WIRES BROKEN IN THE CONNECTOR. THE CONNECTOR WAS REPLACED AND THE SYSTEM RETURNED TO NORMAL OPERATION.
- [SDR DALA2014081204442](https://openairdocs.org/sdr/DALA2014081204442.md): Battery Pack · inoperative · Aug 10, 2014 · N933DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN ROWS 14-22 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA14006910933](https://openairdocs.org/sdr/DALA14006910933.md): Shear Tie · corroded · Feb 1, 2014 · N933DL · Doug MD88 · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED BS 1830 & L14L. REPAIRED IAW ER/A 522746-14 REV ORIG.
- [SDR DALA14006900933](https://openairdocs.org/sdr/DALA14006900933.md): Skin · cracked · Jan 31, 2014 · N933DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED IN TWO PLACES BETWEEN L13-14L BS 1380. HFEC CHECKED IAW NDTSPM 06-10-01.001. REPAIRED IAW PRI 522688-14, REV 0.
- [SDR DALA14006160933](https://openairdocs.org/sdr/DALA14006160933.md): Receptacle · worn · Jan 28, 2014 · N933DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT BOTH THE LT UPPER AND THE RT UPPER RELEASE SPADE RECEPTACLE FOR THE TAILCONE WERE WORN OUT OF ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORI
- [SDR DALA14006150933](https://openairdocs.org/sdr/DALA14006150933.md): Cam · damaged · Jan 28, 2014 · N933DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS MISSING HARDWARE; WHICH CAUSED IT TO BE OUT OF ALLOWABLE RIG LIMITS, EXCESSIVE FORE & AFT PLAY. THE CAM BASE WAS REPLACED AND MISSING SPACERS/SHIMS WERE THEN INSTALLED. THE SYSTEM WAS RI

Next page: https://openairdocs.org/deregistered/N933DL-2019-09-16/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 n_number = 'N933DL' AND deregistration_id = 'N933DL-2019-09-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N933DL-2019-09-16/reports

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