# Service difficulty reports: N906DE, cancelled Nov 29, 2022

A list on [N906DE, cancelled Nov 29, 2022](https://openairdocs.org/deregistered/N906DE-2022-11-29.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 3 · 122 reports

- [SDR DALA2020030601658](https://openairdocs.org/sdr/DALA2020030601658.md): Smoke Detector · false activation · Mar 6, 2020 · N906DE · Doug MD88 · Smoke Detection
  > L1 LAVATORY SMOKE ALARM SOUNDED ON AFTER HOT WATER WAS POURED IN SINK. NO SMOKE OR FIRE DETECTED. R/R FWD LAV SMOKE DET PER MD88 AMM 26-13. CHECKS NML. OK FOR SVC. (LP6616168)
- [SDR DALA2020021801212](https://openairdocs.org/sdr/DALA2020021801212.md): Switch · shorted · Feb 17, 2020 · N906DE · Doug MD88 · Door Warning System
  > TAIL CONE UNSAFE ON LANDING. T/S PER MD88 WDM 52-73-11. FOUND TAILCONE LOCKING ANNUNCIATOR OUTSIDE SWITCH 51-537 GROUNDING OUT AND GENERATING FAULT. R/R TAILCONE EXTERNAL WARNING SWITCH, CK GOOD. (LP6411596)
- [SDR DALA2020021701177](https://openairdocs.org/sdr/DALA2020021701177.md): Connector · dirty · Feb 16, 2020 · N906DE · Doug MD88 · Fuselage Main, Bulkhead Fuselage wiring
  > TAILCONE UNSAFE ON OAP AFTER LANDING. T/S AFT TAIL CONE INDICATION WITH REF TO MD88 SSM 53-52. NO ABNORMAL INDICATION ON I/B TO RDU. DID FIND TAIL CONE LOCKING OUTSIDE SWITCH WITH DE-ICE FLUID IN CONNECTOR. CLEANED CONNECTOR AND EXERCISED OUTSIDE SWITCH. NO IN
- [SDR DALA2020021401134](https://openairdocs.org/sdr/DALA2020021401134.md): Warning Message · false activation · Feb 13, 2020 · N906DE · Doug MD88 · Door Warning System
  > TAILCONE UNSAFE MSG ON OAP. TAILCONE SWITCHES INSPECTED TAILCONE CABLES AND PINS.ALL CHECK GOOD.DOOR DECAL IS NOT PUNCTURED.OK FOR SERVICE. (LP6411572)
- [SDR DALA2020011600324](https://openairdocs.org/sdr/DALA2020011600324.md): Longeron · damaged · Jan 15, 2020 · N906DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > LONGERON 24LT DAMAGED AT STA 1295. SPLICED IN NEW SECTION REF MD88 SRM 53-02 FIG 18 SHEET 2. (LP1447541)
- [SDR DALA2020011400242](https://openairdocs.org/sdr/DALA2020011400242.md): Charger · inoperative · Jan 14, 2020 · N906DE · Doug MD88 · Emergency Lighting
  > TAIL CONE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED B5-28 BATTERY CHARGER IN REF MD88 AMM 33-53 -00. OPS CHECK GOOD. (LP1444634)
- [SDR DALA2019102706183](https://openairdocs.org/sdr/DALA2019102706183.md): Battery Pack · inoperative · Oct 26, 2019 · N906DE · Doug MD88 · Emergency Lighting
  > FOUND ROWS 1-4 CIELING EMERGENCY LIGHTS INOP. R&R BATTERIES AT BATTERY PACK B5-100. CHECKS OK. A/C OK FOR SVC. REF MD-88 AMM 33-53. (LP5587492)
- [SDR DALA2019102906267](https://openairdocs.org/sdr/DALA2019102906267.md): Fairing · missing · Oct 13, 2019 · N906DE · Doug MD88 · Trailing Edge Flaps
  > RH WING INBOARD FLAP HINGE SECONDARY FAIRING MISSING. INSTALLED RT WING FLAP TRACK FAIRING PER ERA 580914-14 REV ORIGINAL. (LP5587434)
- [SDR DALA2019090105104](https://openairdocs.org/sdr/DALA2019090105104.md): B-Nut · loose · Aug 30, 2019 · N906DE · Doug MD88 · Hydraulic System, Main
  > ON POST FLIGHT FOUND MORE RESIDUAL FLUID ENTERING APU FWD NON RAM DOOR INLET. AFTER ENGS SHUT DOWN AND APU SUPPLY TO PACKS NOTICED BURNING OIL ODOR IN COCKPIT COMPLETED A/C SMOKE FUME QUESTIONNAIRE. INSPECTED FOR LEAKS AROUND TAIL COMP, SPUN ENGINES, RAN THRUS
- [SDR DALA2019071704274](https://openairdocs.org/sdr/DALA2019071704274.md): Battery · discharged · Jul 17, 2019 · N906DE · Doug MD88 · Emergency Lighting
  > THE AFT OVERWING UPPER EXIT LIGHTS WENT INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES B5-105 PER AMM 33-53. OPERATION IS NOW NORMAL. (LP #5773704)
- [SDR DALA2019031201622](https://openairdocs.org/sdr/DALA2019031201622.md): Light · disconnected · Mar 12, 2019 · N906DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT OUT AT SEAT 33 E&D. FOUND LIGHT UNPLUGGED. CONNECTED SAME. CHECKS GOOD OK FOR SVC. (LP5765822)
- [SDR DALA2019031201621](https://openairdocs.org/sdr/DALA2019031201621.md): Battery · discharged · Mar 12, 2019 · N906DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS INOP IN OVERHEAD FROM SEAT 11-14. R/R BATTERIES FOR OVERHEAD LIGHTS 11-14. PER AMM 33-53. CHECKS NRML. OK FOR SVC. R/R BATTERIES FOR OVERHEAD LIGHTS 11-14. PER MD88 AMM 33-53. CHECKS NRML. OK FOR SVC. (LP5765823)
- [SDR DALA2018111206598](https://openairdocs.org/sdr/DALA2018111206598.md): Doubler · worn · Nov 10, 2018 · N906DE · Doug MD88 · Cargo/Baggage Doors
  > WEAR ON EXTERNAL REPAIR DOUBLERS AT FWD/ AFT LOWER CORNER OF FWD CARGO DOOR. EXTERNAL REPAIR DOUBLERS AT FWD/ AFT LOWER EDGE CORNERS WERE REPLACED PER ER/A 486624-14MA REV ORIGINAL.
- [SDR DALA2018091405593](https://openairdocs.org/sdr/DALA2018091405593.md): Wire Harness · defective · Sep 13, 2018 · N906DE · Doug MD88 · Light System Wiring
  > AISLE SEAT EMERGENCY LIGHTS INOP 23D AND 33D. REPLACED WIRING HARNESS UNDER SAET 23D AND REPLACED LIGHT ASSEMBLY ON 33D REF AMM 33-53.
- [SDR DALA2018090905505](https://openairdocs.org/sdr/DALA2018090905505.md): Light · inoperative · Sep 9, 2018 · N906DE · Doug MD88 · Emergency Lighting
  > LEFT EXTERIOR EMERGENCY LIGHT IS OUT. R&R LT EMERGENCY EXTERIOR LIGHT IAW AMM 33-41, OP CKS GOOD.
- [SDR DALA2018060503809](https://openairdocs.org/sdr/DALA2018060503809.md): Smoke Detector · faulty · Jun 4, 2018 · N906DE · Doug MD88 · Smoke Detection
  > AFT LEFT LAVATORY SMOKE DETECTOR SOUNDING UPON ARRIVAL IN ATL. NO SMOKE FOUND. REPLACED AFT LEFT SMOKE DETECTOR PER AMM 26-21.
- [SDR DALA2018022601128](https://openairdocs.org/sdr/DALA2018022601128.md): Connector · disconnected · Feb 24, 2018 · N906DE · Doug MD88 · Light System Wiring
  > ON SVC CK FOUND EMERGENCY LIGHT OUT, ROW 26. FOUND PLUG DISCONNECTED UNDER SEAT RECONNECTED. CKS OK.
- [SDR DALA2018013100517](https://openairdocs.org/sdr/DALA2018013100517.md): Connector · disconnected · Jan 29, 2018 · N906DE · Doug MD88 · Light System Wiring
  > EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:13D INTERIOR. FOUND CONNECTOR UNPLUGGED, RE-CONNECTED OPS NML.
- [SDR DALA2018011800287](https://openairdocs.org/sdr/DALA2018011800287.md): Battery Pack · inoperative · Jan 18, 2018 · N906DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS IN FIRST CLASS CEILING INOPERATIVE. REPLACED THE BATTERY PACK B5-100 IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA2017100207232](https://openairdocs.org/sdr/DALA2017100207232.md): Lamp · inoperative · Sep 30, 2017 · N906DE · Doug MD88 · Emergency Lighting
  > RT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-50.
- [SDR DALA2016092406823](https://openairdocs.org/sdr/DALA2016092406823.md): Skin · cracked · Sep 23, 2016 · N906DE · Doug MD88 · Trailing Edge Flaps
  > DAMAGE TO CRACKED UPPER SKIN, FORWARD OTBD STUD AREA, AT LT OTBD FLAP MID GUIDE VANE. LEFT OTBD FLAP MID GUIDE VANE WAS REPAIRED BY ER/A 550294-14, REV ORIGINAL.
- [SDR DALA2016092206778](https://openairdocs.org/sdr/DALA2016092206778.md): Pan · cracked · Sep 21, 2016 · N906DE · Doug MD88 · Cargo/Baggage Doors
  > AWR: HIDDEN DAMAGE, CRACK ON INNER PAN BELOW PRESSURE SEAL AT STOP FITTING 1 AFT EDGE. THIS CARD WAS ATTENDED IAW ER/A 550269-14, REV ORIGINAL AND ETI-88-16-325.
- [SDR DALA2016092206777](https://openairdocs.org/sdr/DALA2016092206777.md): Heater Blanket · cracked · Sep 21, 2016 · N906DE · Doug MD88 · Airfoil Anti/De-ice System
  > INITIAL, CRACK ON RT WING HEATER BLANKET AFT EDGE. CRACK WAS REPAIRED IAW ER/A 494597-14AD MA, REV A. CRACK WAS REPAIRED IAW ER/A 494597-14AD MA REV A.
- [SDR DALA2016092206776](https://openairdocs.org/sdr/DALA2016092206776.md): Heater Blanket · cracked · Sep 21, 2016 · N906DE · Doug MD88 · Airfoil Anti/De-ice System
  > INITIAL, CRACK ON RT WING HEATER BLANKET AFT EDGE. CRACK WAS REPAIRED IAW ER/A 494597-14AD MA, REV A.
- [SDR DALA2016092106757](https://openairdocs.org/sdr/DALA2016092106757.md): Skin · worn · Sep 20, 2016 · N906DE · Doug MD88 · Wing, Plate/Skin
  > WORN PRODUCTION DOUBLER AND INTERNAL WING SKIN BETWEEN STA XW=540 TO STA XW=550, AT LT WING VENT BOX. DAMAGE WAS REMOVED IAW ER/A 094477-14, REV A.
- [SDR DALA2016092106755](https://openairdocs.org/sdr/DALA2016092106755.md): Pan · cracked · Sep 20, 2016 · N906DE · Doug MD88 · Cargo/Baggage Doors
  > INITIAL, CRACKED PAN BELOW STOP FITTING 1 AND 2 AT FWD CARGO COMPARTMENT DOOR AFT EDGE. THIS CARD WAS ATTENDED IAW ER/A 550269-14, REV ORIGINAL.
- [SDR DALA2016092106752](https://openairdocs.org/sdr/DALA2016092106752.md): Structure · cracked · Sep 20, 2016 · N906DE · Doug MD88 · Wing, Plate/Skin
  > INITIAL, AD, CRACKED AND SHEARED RIVET ON UPPER BEAVER TAIL STA XW=47 AT LT WING. SHEARED FASTENER WAS REPLACED IAW SRM 51-30-2 AND CRACK.656" WAS REPAIRED IAW ER/A 550300-14, REV: ORIGINAL AND ETI-88-16-341, REV: ORIGINAL.
- [SDR DALA2016092006739](https://openairdocs.org/sdr/DALA2016092006739.md): Scuff Plate · cracked · Sep 19, 2016 · N906DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED AND ELONGATED HOLES AT AFT CARGO DOOR SCUFF PLATE. ELONGATE HOLES AND CRACKS WERE WELDED, HOLES WERE RE-DRILLED AND AREAS WERE GROUND, FPI WAS ACCOMPLISHED ON WELDED AREAS, NO CRACKS WERE FOUND IAW ER/A 491023-14MA, REV A.
- [SDR DALA2016091906707](https://openairdocs.org/sdr/DALA2016091906707.md): Stringer · cracked · Sep 18, 2016 · N906DE · Doug MD88 · Wing, Longeron/Stringer
  > CRACK ON STRINGER 17 RT ON STA XCW=12 INSIDE CENTER TANK. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM THE FORM 8100-9 APPROVAL DATE: 7-SEP-16. AN ADDITIONAL ERA REVISION IS REQUIRED FOR CONTINUED REVENUE SERVICE BEYOND THIS LIMIT, IAW ERA 549279-14, REV ORI
- [SDR DALA2016091906711](https://openairdocs.org/sdr/DALA2016091906711.md): Hinge · damaged · Sep 17, 2016 · N906DE · Doug MD88 · Cargo/Baggage Doors
  > AWR, HIDDEN DISCREPANCY. ELONGATED HOLES ON FWD & AFT HINGE, BOLT AND SPRING AREA, AT AFT CARGO COMPARTMENT DOOR. AFT CARGO COMPARTMENT DOOR HINGES WERE REMOVED IAW AMM 52-30-02, REPAIRED IAW ER/A 497387-14MA, REV B AND REPAIRED HINGES WERE INSTALLED IAW AMM
- [SDR DALA2016091906710](https://openairdocs.org/sdr/DALA2016091906710.md): Hinge · damaged · Sep 17, 2016 · N906DE · Doug MD88 · Cargo/Baggage Doors
  > INITIAL: ELONGATED HOLES ON HINGE 2 EA AT MID CARGO COMPARTMENT DOOR. FWD AND AFT MID CARGO DOOR HINGES WERE REMOVED IAW AMM 52-31-02-201. REPAIRED IAW ER/A 497387-14MA AND ER/A 10521061-14, REV ORIGINAL. REPAIRED HINGES WERE INSTALLED IAW AMM 52-31-02-201.
- [SDR DALA2016091806704](https://openairdocs.org/sdr/DALA2016091806704.md): Intercostal · corroded · Sep 17, 2016 · N906DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL JUST AROUND NUT PLATES STA Y=1307 TO Y=1322 BETWEEN LONG 27LT -28 LT AT AFT CARGO COMPARTMENT. INTERCOSTAL STA Y=1307 TO Y=1322 BETWEEN LONGERON 27LT -28 LT AT AFT CARGO COMPARTMENT WAS REPLACED IAW SRM 51-30-2 AND 51-10-3 PAR 21 AND
- [SDR DALA2016091306602](https://openairdocs.org/sdr/DALA2016091306602.md): Splice · cracked · Sep 12, 2016 · N906DE · Doug MD88 · Wing Miscellaneous Structure
  > INITIAL: CRACKED SPLICE STA XFS=194 AT RT WING L/E STRUCTURE. CRACK.265" WAS REPAIRED IAW ER/A 379404-14MA, REV A.
- [SDR DALA2016091306578](https://openairdocs.org/sdr/DALA2016091306578.md): Intercostal · corroded · Sep 12, 2016 · N906DE · Doug MD88 · Fuselage Miscellaneous Structure
  > AWR: CORROSION ON INTERCOSTAL STA Y=769-Y=788 BETWEEN LONGERON 27 LT AND 28 LT LONG AT MID CARGO COMPARTMENT. INTERCOSTAL WAS REPAIRED IAW SRM 51-70-5, FIG 1.
- [SDR DALA2016091406604](https://openairdocs.org/sdr/DALA2016091406604.md): Frame · cracked · Sep 11, 2016 · N906DE · Doug MD88 · Fuselage Main, Frame
  > INITIAL, CRACKED FRAME STA Y=1510 UPPER SECTION, LOWER RT/LT SECTION AT AFT ACCESSORY COMPARTMENT. FRAMES SECTIONS Y=1510 UPPER CENTRAL AND LOWER RT/LT WERE REPLACED IAW DWG 9911843, REV C.
- [SDR DALA2016091206569](https://openairdocs.org/sdr/DALA2016091206569.md): Longeron · corroded · Sep 11, 2016 · N906DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > INITIAL: CORROSION ON LONGERON NR 20 RT STA Y=1250-1271 AT AFT CARGO COMPARTMENT. SECTION DAMAGE OF LONGERON WAS REMOVED IAW SRM 53-02, FIG 18. SPLICE WAS FABRICATED IAW SRM 53-02, FIG 18. NEW SECTION LONGERON WAS DRILLED AND ADJUSTED IAW SRM 51-10-4. FPI
- [SDR DALA2016091106519](https://openairdocs.org/sdr/DALA2016091106519.md): Beam · cracked · Sep 10, 2016 · N906DE · Doug MD88 · Passenger/Crew Doors
  > INITIAL: DOOR CRACKED L1 DOOR BEAM 1 FWD/AFT FITTINGS. DAMAGE BEAM WERE REPAIRED IAW SRM 52-05, FIG 81.
- [SDR DALA2016091006518](https://openairdocs.org/sdr/DALA2016091006518.md): Repair · worn · Sep 9, 2016 · N906DE · Doug MD88 · Fuselage Miscellaneous Structure
  > INITIAL, WORN PREVIOUS REPAIR ON WEB BETWEEN STA Y=629 TO 636 BETWEEN LONG PROJECTION 27 RT TO 28 RT AT MID CARGO COMPARTMENT. PREVIOUS REPAIR WAS REPLACED IAW SRM 53-01, FIG 2.
- [SDR DALA2016091006517](https://openairdocs.org/sdr/DALA2016091006517.md): Frame · cracked · Sep 9, 2016 · N906DE · Doug MD88 · Fuselage Main, Frame
  > INITIAL CRACKED WEB ON FRAME STA Y= 1485, CANT POSITION 10 HRS AT AFT ACCESSORY COMPARTMENT. WEB ON FRAME STA Y=1485, CANT POSITION 10 HRS AT AFT COMPARTMENT WAS REPAIRED IAW SRM 53-03D, FIG 48, PAR 43.
- [SDR DALA2016091006515](https://openairdocs.org/sdr/DALA2016091006515.md): Skin · cracked · Sep 9, 2016 · N906DE · Doug MD88 · Passenger/Crew Doors
  > DOOR CRACKED L1 DOOR EXTERNAL SKIN LOWER/AFT SECTION. SN 00696 CRACK ON EXTERNAL SKIN LOWER AFT SECTION WAS REPAIRED IAW SRM 52 05D, FIG 37.
- [SDR DALA2016091006514](https://openairdocs.org/sdr/DALA2016091006514.md): Tab · dented · Sep 9, 2016 · N906DE · Doug MD88 · Elevator, Tab Structure
  > DAMAGE T-DENT ON RT ELEVATOR GEARED TAB. RT ELEVATOR GEARED TAB WAS REPAIRED IAW SRM 55-04, P 4.
- [SDR DALA2016091006513](https://openairdocs.org/sdr/DALA2016091006513.md): Frame · cracked · Sep 9, 2016 · N906DE · Doug MD88 · Wing, Rib/Bulkhead
  > A CRACK WAS FOUND ON LT WING FRAME STR 11 OF 1.250" AT STA XRS=160. LT WING FRAME STR 11 WITH CRACK 1.250" WAS REPAIRED WITH CARD 5712-01030-03.
- [SDR DALA2016091006512](https://openairdocs.org/sdr/DALA2016091006512.md): Web · worn · Sep 9, 2016 · N906DE · Doug MD88 · Passenger/Crew Doors
  > DOOR WEAR L1 DOOR WEB AT BEAM 5 AFT SECTION, SN 00698. WEB ON BEAM 5 AFT SECTION WAS REPAIRED IAW SRM 52-01, FIG 4.
- [SDR DALA2016090906485](https://openairdocs.org/sdr/DALA2016090906485.md): Longeron · cracked · Sep 8, 2016 · N906DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > RE-WRITE: INITIAL, CRACKED END LONGERON 2 RT STA Y=1418 AT AFT ACCESSORY COMPARTMENT. REASON FOR RE-WRITE: LONGERON AND END LONGERON NOT INSTALLED. LONGERON AND LONGERON END WERE INSTALLED IAW SRM 51-30-5 AND 53-02, FIG 18.
- [SDR DALA2016090906483](https://openairdocs.org/sdr/DALA2016090906483.md): Pan · cracked · Sep 8, 2016 · N906DE · Doug MD88 · Cargo/Baggage Doors
  > INITIAL, CRACK ON INNER PAN, BEAM NR 1 FWD EDGE AT MID CARGO COMPARTMENT DOOR C2. INNER PAN WAS REPAIRED IAW SRM 52-03D, FIG 8.
- [SDR DALA2016090906478](https://openairdocs.org/sdr/DALA2016090906478.md): Longeron · cracked · Sep 8, 2016 · N906DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > INITIAL, CRACKED LONG 4 LT AND 5 LT STA Y=1437 AT AFT ACCESSORY COMPARTMENT. LONGERONS 4 LT AND 5 LT STA Y=1437 WERE REPAIRED IAW SRM 53-02, FIGURE 18.
- [SDR DALA2016090906481](https://openairdocs.org/sdr/DALA2016090906481.md): Frame · cracked · Sep 7, 2016 · N906DE · Doug MD88 · Fuselage Main, Frame
  > INITIAL, CRACKED FRAME STA Y=1452, LONGERON 8RT AT AFT ACCESSORY COMPARTMENT. FRAME WAS REPLACED IAW DWG 9911860-3, REV L.
- [SDR DALA2016090806466](https://openairdocs.org/sdr/DALA2016090806466.md): Skin · damaged · Sep 7, 2016 · N906DE · Doug MD88 · Elevator, Plate/Skin
  > DENT AND SRATCHES ON UPPER SKIN XET=82 AT RT ELEVATOR. AREA WAS FOUND OUT OF LIMITS AND WAS REPAIRED IAW ETI-88-16-327 REVISION 1 AND ER/A 550271-14 REV. ORIGINAL.
- [SDR DALA2016090806463](https://openairdocs.org/sdr/DALA2016090806463.md): Frame · cracked · Sep 7, 2016 · N906DE · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1474, LONGERON 18R AT AFT ACCESSORY COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 51-70-5 FIG. 1.
- [SDR DALA2016090806460](https://openairdocs.org/sdr/DALA2016090806460.md): Floor Panel · cracked · Sep 7, 2016 · N906DE · Doug MD88 · Fuselage Floor Panel
  > CRACK ON CHANNEL OF FLOOR PANEL. THE FLOOR PANEL REPAIRED IAW SRM 53-05 FIG 131B AND 131C, AND SRM 51-70-1 PAG. 10.

Next page: https://openairdocs.org/deregistered/N906DE-2022-11-29/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 = 'N906DE' AND deregistration_id = 'N906DE-2022-11-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N906DE-2022-11-29/reports

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