# Service difficulty reports: N911DE, cancelled Jun 13, 2022

A list on [N911DE, cancelled Jun 13, 2022](https://openairdocs.org/deregistered/N911DE-2022-06-13.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 · 159 reports

- [SDR DALA2020030701695](https://openairdocs.org/sdr/DALA2020030701695.md): Frame · cracked · Mar 7, 2020 · N911DE · Doug MD88 · Fuselage Main, Frame
  > REAR FRAME CRACK AT 0300 POSITION - TAILLCONE MOUNTING FRAME. DRILLED UP NEW FRME P/N 59667694501, READY FOR INSTALLATION. STARTED INSTALLATION OF FRAME IAW MD88 SRM 51-30-02, COMPLETED INSTALLATION OF FRAME PER MD88 SRM 51-30-02. (LP1519804)
- [SDR DALA2020030701694](https://openairdocs.org/sdr/DALA2020030701694.md): Frame · cracked · Mar 7, 2020 · N911DE · Doug MD88 · Fuselage Main, Frame
  > REAR FRAME CRACKED AT 0700 POSITION - TAILCONE MOUNT FRAME. DRILLED UP NEW FRAME P/N 59667691. INSTALLED NEW FRAME PER MD 88 SRM 51-30-02. (LP1519795)
- [SDR DALA2020030701692](https://openairdocs.org/sdr/DALA2020030701692.md): Latch · out of adjust · Mar 7, 2020 · N911DE · Doug MD88 · Aerodynamic Fairings
  > TAILCONE RELEASE TEST FAILED USING AFT BULKHEAD DOOR. ADJUSTED RIGHT UPPER AND LEFT LOWER TAILCONE LATCHES PER MD88 AMM 5353 OPS CHK NML. (LP1519691)
- [SDR DALA2020030701693](https://openairdocs.org/sdr/DALA2020030701693.md): Latch · worn · Mar 4, 2020 · N911DE · Doug MD88 · Aerodynamic Fairings
  > TAILCONE ATTACH LATCH @0800 POSITION LOOSE AND WORN. REPLACED TAILCONE ATTACH LATCH AT 0800 POSITION PER MD88 AMM 53-53 NEEDS ADJUSTMENT AT TAILCONE INST.(481754) TAILCONE LATCH ADJUSTED OPS NML. (LP1519811)
- [SDR DALA2020022501396](https://openairdocs.org/sdr/DALA2020022501396.md): Battery Pack · inoperative · Feb 25, 2020 · N911DE · Doug MD88 · Emergency Lighting
  > OVERHEAD EMER LIGHTS OUT FROM SEATS 11-15. R/R EMER BATT PACK BATTERIES PER MD88 AMM 33-53. (LP6465677)
- [SDR DALA2019042502628](https://openairdocs.org/sdr/DALA2019042502628.md): Connector · disconnected · Apr 24, 2019 · N911DE · Doug MD88 · Light System Wiring
  > FOUND EMERGENCY LIGHTS OUT ON SEAT 35 DE AND 25 DE. RECONNECTED THE QUICK DISCONNECTS ON THE EMERGENCY LIGHTS FOR SEATS 25 AND 35 DE. OPS CHECK GOOD. (LP4893432)
- [SDR DALA2019040202076](https://openairdocs.org/sdr/DALA2019040202076.md): Cable · torn · Apr 2, 2019 · N911DE · Doug MD88 · Aerodynamic Fairings
  > AWR IN REFERENCE AMDS 5350-4287 STEP 4 TORN ON TAILCONE KEVLAR CABLE WAS FOUND. KEVLAR CABLE WAS REPLACED PER MD-88 AMM 20-30-01 AND MD-88 AMM 20-10-17-201. (LP1012703)
- [SDR DALA2019040202075](https://openairdocs.org/sdr/DALA2019040202075.md): Doubler · corroded · Apr 1, 2019 · N911DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON PRODUCTION DOUBLER AT AFT LAVATORY PANEL. DUE TO CORROSION OUT OF LIMITS PRODUCTION DOUBLER AT AFT LAVATORY PANEL WAS REPAIRED AS A TIME LIMITED REPAIR PER ETI-88-19-027 REV. 3 AND ER/A 576847-14 REV. ORIG SECTION I. MAINTENANCE REQUIREMENTS WERE
- [SDR DALA2019033002043](https://openairdocs.org/sdr/DALA2019033002043.md): Skin · damaged · Mar 30, 2019 · N911DE · Doug MD88 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION: CREASE ON FUSELAGE SKIN BTW STA Y=1265 AND Y =1277 BTW LONG 27L AND 28R. FUSELAGE SKIN BTW STA Y=1265 AND Y=1277 BTW LONG 27L AND 28R WAS REPAIRED PER ER/A 576844-14 REV.: ORIG. SEC.: I AND ETI-88-19-030 REV: ORIG. ACCOMPLISH SECTION II REP
- [SDR DALA2019032901991](https://openairdocs.org/sdr/DALA2019032901991.md): Paint · damaged · Mar 28, 2019 · N911DE · Doug MD88 · Rudder, Tab Structure
  > INITIAL INSPECTION: MISSING AND DAMGE PAINT ON RUDDER CONTROL TAB. TAB WAS REMOVED/INSTALLED PER AMM 27-20-02-401. PAINTED PER P.S. 900-3-6-NO36 AND BALANCED PER SRM 55-40-01. (LP1006583)
- [SDR DALA2019033102056](https://openairdocs.org/sdr/DALA2019033102056.md): Skin · dented · Mar 27, 2019 · N911DE · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN STA Y=1250-1287 & L27L TO L28R DENTS & SCRATCHES. ACCOMPLISH ER/A 576844-14 SECTION II INSPECTION WITHIN EVERY 8000 CYCLES AFTER ACCOMPLISHMENT OF THE SECTION I REPAIR. (LP1007252)
- [SDR DALA2019033102055](https://openairdocs.org/sdr/DALA2019033102055.md): Skin · damaged · Mar 26, 2019 · N911DE · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AFT LAV SERVICE DOOR CUTOUT STA Y=1307-1322, L-22L SKIN & INTERNAL DOUBLER/ CORROSION. ACCOMPLISH ER/A 576847-14 SECTION II INSPECTION WITHIN EVERY 3000 CYCLES UNTIL SECTION III IS ACCOMPLISHED WITHIN 8000, ALL AFTER ACCOMPLISHMENT OF SECTION I.
- [SDR DALA2019010200014](https://openairdocs.org/sdr/DALA2019010200014.md): Coalescer Bag · dirty · Jan 1, 2019 · N911DE · Doug MD88 · Humidity Control System
  > AFTER T/O AND GEAR RETRACTION STRONG SMELL FROM NOSE TIRES NOTICED IN FLT DECK AND MAIN CABIN. C/W ODI SMOKE /ODOR T/S WC 2120-2367 PERFORMED ALTERNATE DUCT BURNOUT PER WC4950-2215 AND COALESCE BAGS REPLACED PER WC2170-4139 COULD NOT DUPLICATE ODOR[428838] REF
- [SDR DALA2018051603379](https://openairdocs.org/sdr/DALA2018051603379.md): Warning System · false activation · May 14, 2018 · N911DE · Doug MD88 · Ground Proximity System
  > DUE TO EMERGENCY DECLARED BECAUSE OF TOO LOW GEAR AURAL WARNING FOR GEAR WARNING DURING APPROACH. T/S THE EGPWS AND RADIO ALTIMETER SYSTEMS PER AMM 34-45 AND 34-42 RESPECTIVELY. CHECK ALL ANTENNA CONNECTIONS FOR CORROSION AND SECURITY.FINDINGS.
- [SDR DALA2018043002896](https://openairdocs.org/sdr/DALA2018043002896.md): Slide · torn · Apr 29, 2018 · N911DE · Doug MD88 · Escape Slide
  > SERVICE DOOR SLIDE NOTED TO BE TORN. REPLACED R1 SLIDE PACK.
- [SDR DALA2018040402179](https://openairdocs.org/sdr/DALA2018040402179.md): Door Frame · dirty · Apr 4, 2018 · N911DE · Doug MD88 · Fuselage Main, Structure
  > FORCE REQUIRED TO OPEN THE DOOR AND DROP THE TAILCONE. AFT PASSENGER DOOR OUT OF LIMITS IAW AMDS 88- 0553-8-0066, AMDS 5350-01077-0101 STEP 7. CLEANED DEBRIS FROM THE DOOR OPENING AND CABLES WERE LUBRICATED. CABLE ASSY RECHECKED, DOOR OPEN FORCE FOUND
- [SDR DALA2018010300035](https://openairdocs.org/sdr/DALA2018010300035.md): Battery · discharged · Jan 2, 2018 · N911DE · Doug MD88 · Emergency Lighting
  > EMERGENCY CEILING LIGHTS IN TAIL INOP. BATTERIES WOULD NOT HOLD CHARGE. CHANGED 'D' CELL BATTERIES OPERATIONAL CHECK OF TAIL PATH CEILING LIGHTS GOOD IAW AMM 33-50. P/N AD-4002P.
- [SDR DALA2017081506259](https://openairdocs.org/sdr/DALA2017081506259.md): Unknown · odor · Aug 13, 2017 · N911DE · Doug MD88 · Air Distribution System
  > DIVERTED DUE TO A REPORTED SWEET BURNING ODOR FROM OVERHEAD BINS AT SEAT ROWS 12 TO 20. NO ODOR WAS PRESENT IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT INTERIOR, THE OVERHEAD LIGHT BALLAST AND THE AREA ABOVE THE PSUS. THE RECIRCULATION FAN AND THE BAG
- [SDR DALA2017052704330](https://openairdocs.org/sdr/DALA2017052704330.md): Wire · broken · May 27, 2017 · N911DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTING INOPERATIVE AT 24DE. FOUND WIRE BROKEN ON HARNESS. REPAIRED THE WIRE HARNESS IAW SWPM 20. ALL LIGHTS OPS CHECKED GOOD IAW AMM 33-53.
- [SDR DALA2017052704329](https://openairdocs.org/sdr/DALA2017052704329.md): Battery Pack · inoperative · May 27, 2017 · N911DE · Doug MD88 · Emergency Lighting
  > EMERGENCY CEILING LIGHTS INOPERATIVE BETWEEN ROWS 26 AND 30. REPLACED THE BATTERIES AT ROW 28. OPS CHECKED GOOD IAW AMM 33-53.
- [SDR DALA2017050803634](https://openairdocs.org/sdr/DALA2017050803634.md): Connector · broken · May 6, 2017 · N911DE · Doug MD88 · Light System Wiring
  > DURING SERVICE CHECK, FOUND SEAT 22 EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR BROKEN. INSTALLED A NEW CONNECTOR IAW SWPM 20. OPS CHECKED OK. OK FOR SERVICE.
- [SDR DALA2017050803633](https://openairdocs.org/sdr/DALA2017050803633.md): Wire · broken · May 6, 2017 · N911DE · Doug MD88 · Light System Wiring
  > DURING SERVICE CHECK, FOUND AFT CATWALK MIDDLE EMERGENCY LIGHT INOPERATIVE. WIRE BROKEN FROM CONNECTOR. INSTALLED NEW TERMINAL PIN IAW SWPM 20. OPS CHECKED OK. OK FOR SERVICE.
- [SDR DALA2017050203523](https://openairdocs.org/sdr/DALA2017050203523.md): Coffeemaker · malfunctioned · May 1, 2017 · N911DE · Doug MD88 · Buffet/Galleys
  > ON ENTERING THE ACFT, A STRONG ELECTRICAL BURNING ODOR. TROUBLESHOT IAW IAW 2120-2367. FOUND F/C FWD NR 1 COFFEEMAKER HEATING WITH SWITCH IN OFF POSITION CREATING A BURNING ODOR. R & R THE COFFEEMAKER AND TESTED IAW AMM 25-36. OPS OK. NO ODOR. OK FOR S
- [SDR DALA2017030201713](https://openairdocs.org/sdr/DALA2017030201713.md): Release Cable · broken · Mar 1, 2017 · N911DE · Doug MD88 · Aerodynamic Fairings
  > AFT ACCESSORIES COMPARTMENT: BROKEN RELEASE TAILCONE CONTROL CABLE WIRES AT 10 HRS POSITION. RELEASE TAILCONE CONTROL CABLE AT 10 HRS POSITION WAS REPLACED AND ADJUSTED PER AMM 20-10-17-201 AND PER AMM 53-53-00-501.
- [SDR DALA2017030101644](https://openairdocs.org/sdr/DALA2017030101644.md): Outflow Valve · cracked · Feb 26, 2017 · N911DE · Doug MD88 · Pressure Regulator/Outflow Valve
  > CRACK ON OUTFLOW VALVE BUTTERFLY. DAMAGED OUTFLOW BUTTERFLY VALVE WAS REMOVED IAW AMM 21-32-05 401.
- [SDR DALA2017022701583](https://openairdocs.org/sdr/DALA2017022701583.md): Rib · cracked · Feb 26, 2017 · N911DE · Doug MD88 · Leading Edge Devices
  > LEFT WING HAD A CRACKED RIB ON SLAT PANEL NR 3 AT XOS 332. THE SLAT PANEL WAS REPLACED, INSTALLED AND ADJUSTED IAW AMM 27-80-01.
- [SDR DALA2017022701580](https://openairdocs.org/sdr/DALA2017022701580.md): Skin · cracked · Feb 26, 2017 · N911DE · Doug MD88 · Emergency Exits
  > DAMAGE TEE FITTING DURING PERFORMING OF AMDS CARD 5200-2503 STEP 2 (F), ONE CRACK WAS FOUND TO THE LT AFT EMERGENCY EXIT DOOR INNER SKIN. REPAIRED IAW ETI-88-17-075 REV 3 AND ERA 555630-14 REV ORIGINAL.
- [SDR DALA2017022701579](https://openairdocs.org/sdr/DALA2017022701579.md): Pan · cracked · Feb 25, 2017 · N911DE · Doug MD88 · Fuselage Main, Structure
  > CRACK ON RT EMERGENCY EXIT DOOR FRAME PAN UPPER AREA BS 864 TO 880. DAMAGE AREA WAS REPAIRED IAW ETI-88-17-063 REV 5, ER/A 554155-14 REV. ORIG. AND SRM 53-05 FIG 32.
- [SDR DALA2017022601577](https://openairdocs.org/sdr/DALA2017022601577.md): Frame · cracked · Feb 25, 2017 · N911DE · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESORIES COMPARTMENT HAD A CRACKED FRAME BS 1485. THE FRAME WAS REPAIRED IAW SRM 53-03D, FIG 43.
- [SDR DALA2017022601576](https://openairdocs.org/sdr/DALA2017022601576.md): Shear Tie · cracked · Feb 25, 2017 · N911DE · Doug MD88 · Fuselage Internal Mounting Structure
  > AFT ACCESORIES COMPARTMENT HAD A CRACKED SHEAR TIE BS 1380 BETWEEN LONGERONS 17 & 18R. THE SHEAR TIE WAS REPLACED IAW SRM 53-14-4, 51-30-2, AND 51-30-5.
- [SDR DALA2017022601575](https://openairdocs.org/sdr/DALA2017022601575.md): Rib · cracked · Feb 25, 2017 · N911DE · Doug MD88 · Wing, Rib/Bulkhead
  > LEFT WING RIB CRACKED ON FIXED LEADING EDGE APROX XRS 295. THE RIB WAS REPLACED IAW SRM 51-30-2, 51-30-5.
- [SDR DALA2017022301488](https://openairdocs.org/sdr/DALA2017022301488.md): Angle · cracked · Feb 22, 2017 · N911DE · Doug MD88 · Passenger/Crew Doors
  > L1 DOOR HAS A CRACKED ANGLE ON FWD INTERCOSTAL BETWEEN BEAMS 4 AND 5. THE ANGLE WAS REPLACED IAW SRM 51-30-2 AND DWG 9955763 REV. M.
- [SDR DALA2017022301486](https://openairdocs.org/sdr/DALA2017022301486.md): Access Panel · damaged · Feb 22, 2017 · N911DE · Doug MD88 · Wing, Plate/Skin
  > ELONGATED HOLES ON FUEL TANK ACCESS PANEL1365C. REPAIRED IAW SRM 51-22-2A PAR. 6.
- [SDR DALA2017022201453](https://openairdocs.org/sdr/DALA2017022201453.md): Frame · cracked · Feb 21, 2017 · N911DE · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESSORIES COMPARTMENT, CRACKED FRAME ON STA Y=1485 CANT. DAMAGE AREA WAS REPAIRED PER ETI-88-17-065 REV 1 AND ER/A 555626-14 RE ORIG.
- [SDR DALA2017022201451](https://openairdocs.org/sdr/DALA2017022201451.md): Floor Support · corroded · Feb 21, 2017 · N911DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS BTW STA Y=1145 AND Y= 1222 BTW LONG 28 RT AND 29 RT. DUE TO EXCESSIVE CORROSION UPPER FLOOR SUPPORT WAS REPLACED PER SRM 51-30-1, 51-30-2 AND 51-30-5. CORROSION ON LOWER FLOOR SUPPORT WAS ATTENDED WITH NRC 00976.
- [SDR DALA2017022201448](https://openairdocs.org/sdr/DALA2017022201448.md): Cargo Track · corroded · Feb 21, 2017 · N911DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT TIE DOWN TRACK FROM STA Y=1117 TO STA Y=1122 IN AFT CARGO COMPARTMENT. TIE TRACK WAS REPLACED PER DRAWING 5936660 REV BZ AND SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR DALA2017022201447](https://openairdocs.org/sdr/DALA2017022201447.md): Floor Support · corroded · Feb 21, 2017 · N911DE · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, CORROSION ON FLOOR SUPPORT STA Y= 1117 BTW LONG 28LH AND 28 RT. FLOOR SUPPORT WAS REPLACED PER, SRM.51-30-5. (LP2900754)
- [SDR DALA2017021901353](https://openairdocs.org/sdr/DALA2017021901353.md): Finger Doubler · corroded · Feb 18, 2017 · N911DE · Doug MD88 · Fuselage Main, Plate/Skin
  > AFT CARGO BAY HAS CORROSION ON A FINGER DOUBLER BETWEEN LONGERONS 28L AND 28R, BS 1231 - 1271. THE FINGER DOUBLERS WERE REPLACED IAW SRM 53-04-3, FIG. 12.
- [SDR DALA2017021801352](https://openairdocs.org/sdr/DALA2017021801352.md): Doubler · corroded · Feb 17, 2017 · N911DE · Doug MD88 · Fuselage Main, Structure
  > AFT CARGO BAY CORROSION ON PREVIOUS REPAIR DOUBLER OF LOWER DOOR FRAME BEAM. THE REPAIR WAS REPLACED IAW SRM 53-05, FIG 123, ETI-88-17-048 REV. ORIGINAL AND ERA 554139-14 REV. ORIGINAL.
- [SDR DALA2017021701317](https://openairdocs.org/sdr/DALA2017021701317.md): Access Panel · corroded · Feb 16, 2017 · N911DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON FUEL TANK ACCESS PANELS 1410C AND 1303C. THE ACCESS PANELS WERE REPLACED.
- [SDR DALA2017021701312](https://openairdocs.org/sdr/DALA2017021701312.md): Intercostal · cracked · Feb 16, 2017 · N911DE · Doug MD88 · Fuselage Miscellaneous Structure
  > RIGHT MLG WHEEL WELL HAS A CRACKED INTERCOSTAL BELOW THE HYD HAND PUMP. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG 2.
- [SDR DALA2017021701310](https://openairdocs.org/sdr/DALA2017021701310.md): Web · cracked · Feb 16, 2017 · N911DE · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT ACCESORIES COMPARTMENT HAS A CRACKED WEB BS 1437, LONGERIN 8 - 9L. THE WEB WAS REPAIRED IAW ETI-88-17-058 REV 1, AND ER/A 554147-14 REV. ORIG.
- [SDR DALA2017021701308](https://openairdocs.org/sdr/DALA2017021701308.md): Skin · cracked · Feb 16, 2017 · N911DE · Doug MD88 · Wing, Plate/Skin
  > LEFT WING CRACKED ON LOWER SKIN BUTE DOOR, XCW 104. THE BUTE DOOR WAS REPAIRED IAW SRM 51-70-4, FIG 1, 51-30-2 AND 51-30-1.
- [SDR DALA2017021701307](https://openairdocs.org/sdr/DALA2017021701307.md): Floor Panel · corroded · Feb 16, 2017 · N911DE · Doug MD88 · Fuselage Floor Panel
  > METALLIC FLOOR PANEL UNDER FIRST OFICCER SEAT CORRODED. A NEW FLOOR PANEL WAS DRILLED IAW SRM 51-10-4 AND A NEW FLOOR PANEL WAS INSTALLED.
- [SDR DALA2017021601279](https://openairdocs.org/sdr/DALA2017021601279.md): Access Panel · corroded · Feb 15, 2017 · N911DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON FUEL TANK ACCESS NR 1414C RT. FUEL TANK ACCESS NR 1414C WAS REPLACED PER SRM 51-22-2A PAR 6.
- [SDR DALA2017021501238](https://openairdocs.org/sdr/DALA2017021501238.md): Web · corroded · Feb 14, 2017 · N911DE · Doug MD88 · Service Doors
  > ELONGATED HOLE ON WEB ON AFT SERVICE DOOR INNER STRUCTURE. REPAIRED IAW ETI-88-17-060 REV 1 AND ERA 554151-14 REV ORIG.
- [SDR DALA2017021501234](https://openairdocs.org/sdr/DALA2017021501234.md): Web · cracked · Feb 14, 2017 · N911DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED WEB BS 1463, LONGERONS 7 - 8L. THE WEB SECTION WAS REPLACED IAW SRM 53-14-4 FIG 3, AND 51-30-5.
- [SDR DALA2017021401193](https://openairdocs.org/sdr/DALA2017021401193.md): Floor Panel · cracked · Feb 13, 2017 · N911DE · Doug MD88 · Fuselage Floor Panel
  > CRACK ON FLOOR PANEL. THE FLOOR PANEL WAS REPAIRED IAW AMM 25-00-00-801 AND SRM 53-01 FIG. 2.
- [SDR DALA2017021401192](https://openairdocs.org/sdr/DALA2017021401192.md): Cusp Web · corroded · Feb 13, 2017 · N911DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB FROM BS 1117 - 1174, RBL 44 - 60. THE CUSP WEB WAS REPLACED IAW SRM 51-30-2, AND 51-30-5.
- [SDR DALA2017021201165](https://openairdocs.org/sdr/DALA2017021201165.md): Cusp Web · corroded · Feb 11, 2017 · N911DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB FROM STA Y=663 TO STA Y=665U AND BTW X=-54 TO X=-60 PER AND LOWER SURFACE. DAMAGE AREA WAS REPAIRED SRM 53-05 FIG 131 A.

Next page: https://openairdocs.org/deregistered/N911DE-2022-06-13/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 = 'N911DE' AND deregistration_id = 'N911DE-2022-06-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N911DE-2022-06-13/reports

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