# Service difficulty reports: N908DL, cancelled Nov 29, 2022

A list on [N908DL, cancelled Nov 29, 2022](https://openairdocs.org/deregistered/N908DL-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 5 · 243 reports

- [SDR DALA2019110506380](https://openairdocs.org/sdr/DALA2019110506380.md): Stiffener · cracked · Nov 4, 2019 · N908DL · Doug MD88 · Engine Cowling System
  > LT ENGINE NOSE COWL FWD BULKHEAD STIFFNER CRACKED AT 6:00 POSITION. TRANSFERED FROM QC LOG 1113449 TO OM-812 057374 ITEM 2. ENGINE S/N 726933 HAS BEEN REMOVED FROM A/C 0908 AND ITEM TRANSFERED TO OM-812 AND SCEPTRE /FOR IRM. 3000CY REINSPECTION INTERVAL HAS 20
- [SDR DALA2019093005575](https://openairdocs.org/sdr/DALA2019093005575.md): Access Door · broken · Sep 30, 2019 · N908DL · Doug MD88 · Engine Cowling System
  > ON WALK AROUND FOUND STARTER ACCESS DOOR BROKEN OFF ON #2 ENG. R+R STARTER ACESS DOOR REF MD88 AMM 71-10 OK FOR SVC. (LP5587208)
- [SDR DALA2019061903653](https://openairdocs.org/sdr/DALA2019061903653.md): Skin · cracked · Jun 19, 2019 · N908DL · Doug MD88 · Leading Edge Devices
  > NR 3 SLAT HAD A 3 INCH CRACK AT THE AFT O/B EDGE. REMOVED #3 SLAT REF WORKCARD 2700-4224-RH-03 JOB 000-0001. COMPLETED #3 R/H SLAT INSTALL AND ADJUST REF AMDS CARD #2700-4224-RH-03. SLAT, RH INTER OFF 88-2780-9-0008 09502 ON 88-2780-9-0008 00041.
- [SDR DALA2019050802895](https://openairdocs.org/sdr/DALA2019050802895.md): Battery · discharged · May 8, 2019 · N908DL · Doug MD88 · Emergency Lighting
  > CABIN STANDBY LIGHTS BETWEEN STA.1100 AND STA. 1200 INOP WHEN TESTED. REPLACED BATTERIES IN POWER PACK IAW AMM 33-52. CHECKS GOOD. (LP5654060)
- [SDR DALA2019040702265](https://openairdocs.org/sdr/DALA2019040702265.md): Wire · exposed · Apr 6, 2019 · N908DL · Doug MD88 · Ice/Rain Protection System Wiring
  > FO SHOCKED BY WINDOW HEAT WIRE CONNECTORS. FOUND EXPOSED WIRE ON ONE QUICK DISCONNECT CONNECTOR ON FO'S ANTIFOG SLIDING WINDOW. REPAIRED CONNECTO PER SPWM CH 20 AND MD88 WDM 30-44 OPS CKS NML. (LP4694336)
- [SDR DALA2019020600810](https://openairdocs.org/sdr/DALA2019020600810.md): Release Mech · wrong part · Feb 5, 2019 · N908DL · Doug MD88 · Aerodynamic Fairings
  > DURING AFT TAIL CONE FRAME REPLACEMENT FOUND WRONG P/N TAILCONE RELEASE MECHANISM CAM INSTALLED. REMOVED CAM P/N 5961569-1 AND INSTALLED P/N 5961569-501 PER MD88 AMM 53-53-02. (LP0933090)
- [SDR DALA2019020600809](https://openairdocs.org/sdr/DALA2019020600809.md): Frame · cracked · Feb 5, 2019 · N908DL · Doug MD88 · Fuselage Main, Frame
  > CANTED FRAME CRACKED AT TAILCONE ALIGNMENT PIN L/H SIDE JUST ABOVE TAILCONE TORQUE CAM. REMOVED UPPER PORTION OF CANTED FRAME DRILLED NEW UPPER CANTED FRAME BEGAN INSTALL REPLACED UPPER CANTED FRAME F.S. 1510 PER DRWG 5966768 RTEPLACED TAILCONE CAM ASSY PER MD
- [SDR DALA2019012900613](https://openairdocs.org/sdr/DALA2019012900613.md): Battery · discharged · Jan 28, 2019 · N908DL · Doug MD88 · Emergency Lighting
  > AFT O/W EMER EXIT LIGHTS OVER DOORS ARE INOP. REPLACED BATTERIES IN BATTERY PACK B5-105 REF AMM 33-53. OPS CHECK GOOD. (LP5564157)
- [SDR DALA2018101506039](https://openairdocs.org/sdr/DALA2018101506039.md): Battery · discharged · Oct 15, 2018 · N908DL · Doug MD88 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INOP IN CEILING. R/R EMERGENCY BATTERIES IN OVERHEAD BIN AT SEATS 4DC, 17ED, AND 24ED PER AMM 33-53 OPS CK NORMAL OK FOR SVC. (LP5351209)
- [SDR DALA2018083005359](https://openairdocs.org/sdr/DALA2018083005359.md): Battery Pack · inoperative · Aug 29, 2018 · N908DL · Doug MD88 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT WAS OUT ROWS 1 - 4 & 16 - 20. REPLACED BATTERY PACKS B5-100 AND B5-102 IAW AMM 44-53. OPS CHECKED GOOD. AC OK FOR SERVICE.
- [SDR DALA2018062604203](https://openairdocs.org/sdr/DALA2018062604203.md): Unknown · odor · Jun 3, 2018 · N908DL · Doug MD88 · Air Distribution System
  > ON SHORT APPROACH AT 800 AGL, A VERY STRONG, ACRID, ELECTRICAL SMELL IN COCKPIT. NO VISIBLE SMOKE. FLIGHT ATTENDANTS SMELLED NOTHING. VERY SLOW TO DISSIPATE AT GATE. PERFORMED PNEUMATIC DIST CABIN SMOKE/ODOR TROUBLESHOOTING W/C 2120-2367 PER NO-DO ODI PROCEDUR
- [SDR DALA2018051403257](https://openairdocs.org/sdr/DALA2018051403257.md): Slide · damaged · May 12, 2018 · N908DL · Doug MD88 · Escape Slide
  > L1 DOOR SLIDE HAS COME APART. REMOVED AND REPLACED L1 DOOR SLIDE PER WORKCARD 2561-4964 SLIDE, PN OFF 09-2561-9-0011 01159 ON 88-2560-9-0003 03247.
- [SDR DALA2018032501874](https://openairdocs.org/sdr/DALA2018032501874.md): Controller · malfunctioned · Mar 24, 2018 · N908DL · Doug MD88 · Windshield/Door Rain/Ice Removal
  > CENTER WINDSHIELD ANTI FOG SENSOR UNIT OVERHEATED WITH CORRESPONDING ODOR/FUMES. REPLACED CENTER WINDSHIELD & CONTROLLER. REPLACED BURNT SCREW ON WINDOW HEAT TERMINAL. OPERATION CHECKS NORMAL.
- [SDR DALA2018030201320](https://openairdocs.org/sdr/DALA2018030201320.md): Lamp · inoperative · Mar 2, 2018 · N908DL · Doug MD88 · Emergency Lighting
  > DURING A SERVICE CHECK, EMERGENCY OVERHEAD LIGHTS OUT AT ROWS 17 - 21. REPLACED THE LAMPS.
- [SDR DALA2017092607104](https://openairdocs.org/sdr/DALA2017092607104.md): Light · inoperative · Sep 26, 2017 · N908DL · Doug MD88 · Emergency Lighting
  > SEAT 14D EMERGENCY LIGHT INOPERATIVE. REPAIRED THE LIGHT IAW AMM 33-53.
- [SDR DALA2017092507083](https://openairdocs.org/sdr/DALA2017092507083.md): Battery Pack · discharged · Sep 24, 2017 · N908DL · Doug MD88 · Emergency Lighting
  > COCKPIT OVERHEAD DOME/PEANUT LIGHTS INOP. RMVD/RPLD EMERGENCY BATTERY PACK B5-23. OPS CK GOOD. OK FOR SVC PER WDM 33-51.
- [SDR DALA2017071305407](https://openairdocs.org/sdr/DALA2017071305407.md): Battery · discharged · Jul 13, 2017 · N908DL · Doug MD88 · Emergency Lighting
  > OVERWING EXIT FWD POSITION EMERGENCY LIGHTS INOP. REPLACED BATTERYS IN OVERWING BATTERY PACK AS PER AMM 33-53-00 CKS GOOD.
- [SDR DALA2017070705245](https://openairdocs.org/sdr/DALA2017070705245.md): Battery Pack · discharged · Jul 7, 2017 · N908DL · Doug MD88 · Emergency Lighting
  > EMER CEILING LIGHTS INOP FROM ROW 16-20. REPLACED BATTERY PACK AT B5-102 REF AMM 33-53. OPS CHECK GOOD.
- [SDR DALA2017011800433](https://openairdocs.org/sdr/DALA2017011800433.md): Frame · cracked · Jan 17, 2017 · N908DL · Doug MD88 · Fuselage Main, Frame
  > CRACK FOUND IN WEB OF CANTED FRAME BS 1463. REPAIRED IAW PRI 554532-14 REV 0, PRI 554532-14 REV 1, PRI 554532-14 REV 2.
- [SDR DALA2017011700382](https://openairdocs.org/sdr/DALA2017011700382.md): Structure · cracked · Jan 16, 2017 · N908DL · Doug MD88 · Aerodynamic Fairings
  > TAIL CONE INTERIOR CRACKED BOTTOM AFT LEFT SIDE. INSTALLED SERVICEABLE TAIL CONE IAW AMDS TASK CARD 5350-4287. (LP2852835)
- [SDR DALA2017011600373](https://openairdocs.org/sdr/DALA2017011600373.md): Guide · missing · Jan 14, 2017 · N908DL · Doug MD88 · Aerodynamic Fairings
  > TAIL CONE RELEASE CABLE PULLEY MISSING CABLE GUIDE AT 9 O'CLOCK. INSTALLED PULLEY CABLE GUIDE AT 9 O'CLOCK POSITION, O.K. FOR SERVICE.
- [SDR DALA2017011600372](https://openairdocs.org/sdr/DALA2017011600372.md): Latch · damaged · Jan 14, 2017 · N908DL · Doug MD88 · Aerodynamic Fairings
  > TAIL CONE LATCH AT 4 O'CLOCK POSITION MISSING HARDWARE AND LOOSE. INSTALLED MISSING HARDWARE AND TIGHTENED, OK FOR SERVICE.
- [SDR DALA2017010300015](https://openairdocs.org/sdr/DALA2017010300015.md): Pump · failed · Jan 1, 2017 · N908DL · Doug MD88 · Fuel Boost Pump
  > DIVERTED DUE TO THE CIRCUIT BREAKER FOR THE RIGHT WING FORWARD FUEL BOOST PUMP TRIPPED AT FL 330. CREW RECEIVED EOAP MESSAGE RT FUEL INLET PRESSURE LOW AND THE RIGHT WING AFT FUEL BOOST PUMP WAS ON MEL. CREW WAS ABLE TO CROSSFEED FUEL FROM THE LEFT WING TAN
- [SDR DALA2017010100020](https://openairdocs.org/sdr/DALA2017010100020.md): Battery Pack · inoperative · Dec 31, 2016 · N908DL · Doug MD88 · Emergency Lighting
  > MULTIPLE CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED & REPLACED THE BATTERIES. OPS CHECKED GOOD.
- [SDR DALA2016102507565](https://openairdocs.org/sdr/DALA2016102507565.md): Blade · damaged · Oct 24, 2016 · N908DL · Doug MD88 · Turbine Engine Compressor Section
  > RETURNED TO SGF DUE TO NR 1 ENGINE COMPRESSOR STALL WITH A REDUCED THRUST. CABIN CREW VERIFIED COMPRESSOR STALL AND CABIN ODOR. MTC FOUND FAN BLADE TIPS BENT FORWARD INDICATING ENGINE INGESTED SOFT FOD. MTC FOUND 2ND STAGE VANES PULLING FROM CASE. ENGINE W
- [SDR DALA2016092206774](https://openairdocs.org/sdr/DALA2016092206774.md): Wire · out of position · Sep 22, 2016 · N908DL · Doug MD88 · Light System Wiring
  > 1R GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. FOUND WIRES CROSSED BETWEEN 1R DOOR OVERHEAD EMERGENCY LIGHT SOCKET AND SWITCH FOR OVERHEAD WORK LIGHTS. RECONFIGURED WIRING IAW WDM 33-51-12. OPS CHECK GOOD.
- [SDR DALA2015100505957](https://openairdocs.org/sdr/DALA2015100505957.md): Slide · misinstalled · Oct 3, 2015 · N908DL · Doug MD88 · Escape Slide
  > MAINTENANCE FOUND TAIL CONE SLIDE NOT PROPERLY INSTALLED. SLIDE WAS PROPERLY INSTALLED.
- [SDR DALA2015100205902](https://openairdocs.org/sdr/DALA2015100205902.md): Release Cable · broken · Oct 2, 2015 · N908DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE FOUND BROKEN STRANDS ON TAILCONE RELEASE CONTROL CABLE SEGMENT. TAIL CONE RELEASE CONTROL CABLE SEGMENT WAS R & R.
- [SDR DALA2015100205900](https://openairdocs.org/sdr/DALA2015100205900.md): Frame Splice · not reported · Oct 1, 2015 · N908DL · Doug MD88 · Fuselage Main, Frame
  > AFT PRESSURE BULKHEAD LOWER FRAME SPLICES WERE FOUND BETWEEN LONGERON 26R-27R AND BETWEEN LONGERON 26-27L. AREA WAS REPAIRED IAW ER/A 537817-14, REV ORIG.
- [SDR DALA2015100105895](https://openairdocs.org/sdr/DALA2015100105895.md): Structure · broken · Sep 30, 2015 · N908DL · Doug MD88 · Main Landing Gear
  > DURING MAINTENANCE, FOUND BROKEN EDGES AT RT MLG BEARING BORE. REPAIRED IAW ER/A 537816-14AD, REV ORIGINAL.
- [SDR DALA2015100105894](https://openairdocs.org/sdr/DALA2015100105894.md): Skin · damaged · Sep 30, 2015 · N908DL · Doug MD88 · Fuselage Main, Plate/Skin
  > HAD LIGHTNING STRIKE ON FUSELAGE SKIN ABOVE LONGERGON 3R BETWEEN BS 1079-1098. REPAIRED IAW ER/A 537810-14, REV ORIGINAL.
- [SDR DALA2015093005870](https://openairdocs.org/sdr/DALA2015093005870.md): Skin · damaged · Sep 29, 2015 · N908DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING VISUAL INSPECTION IAW ETI-88-15-326, STEP 3, ELONGATED HOLES ON FS=125-133 Z=22 AT LT FUSELAGE SKIN EXISTING REPAIR AREA. AREA WAS REPAIRED IAW ER/A 234659-14, REV E.
- [SDR DALA2015093005869](https://openairdocs.org/sdr/DALA2015093005869.md): Skin · cracked · Sep 29, 2015 · N908DL · Doug MD88 · Fuselage Main, Plate/Skin
  > ONE CRACK 2.937 INCHES IN LENGTH WAS FOUND ON FUSELAGE SKIN AT BS 1418 AND BETWEEN LONGERONS 1 AND 2R. REPAIRED IAW ER/A 537780-14, REV A.
- [SDR DALA2015092905852](https://openairdocs.org/sdr/DALA2015092905852.md): Cargo Track · damaged · Sep 28, 2015 · N908DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > ELONGATED HOLES ON LT CARGO TRACK FROM BS 427 - 522. THE CARGO TRACK WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-3, PAR 21,14 AND ER/A 537819-14, REV ORIGINAL AND 53-05, FIG 49.
- [SDR DALA2015092905851](https://openairdocs.org/sdr/DALA2015092905851.md): Skin · deformed · Sep 28, 2015 · N908DL · Doug MD88 · Service Doors
  > DEFORMED EXTERNAL SKIN ON R1 DOOR LOWER EDGE. R1 DOOR LOWER EDGE WAS REPAIRED IAW ER/A 537815-14, REV. ORIGINAL.
- [SDR DALA2015092805839](https://openairdocs.org/sdr/DALA2015092805839.md): Cargo Track · damaged · Sep 27, 2015 · N908DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > ELONGATED HOLES ON RT CARGO TRACK BS 427 - 522. THE CARGO TRACK WAS REPLACED WITH SRM 51-30-1, 01-30-2, 51-10-4, AN D51-10-3 PAR 14, 21.
- [SDR DALA2015092605833](https://openairdocs.org/sdr/DALA2015092605833.md): Tee Fitting · corroded · Sep 25, 2015 · N908DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION FOUND ON TEE BETWEEN BS 1361 - 1410, LONGERON 24 - 25L IN THE AFT ACCESSORY COMPARTMENT. FOUND TO BE OUT OF LIMITS. THE TEE WAS REMOVED, REPAIRED AND INSTALLED IAW SRM 53-01, FIG 2, SH 4, SRM 51-10-3, PAR 14-21, 51-30-2 AND 51-30-5.
- [SDR DALA2015092205778](https://openairdocs.org/sdr/DALA2015092205778.md): Frame · cracked · Sep 21, 2015 · N908DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME CAP ON BS Y=1418 BETWEEN LONG 1 RT AND 2 RT AT AFT ACCESSORY COMPARTMENT, CAT, SM, IN REF CARD 06, ZONE 65, ZONE 65, CARD 27. FRAME CAP WAS REPLACED IAW SRM 51-30-5, 51-10-3, CRACK 0.800".
- [SDR DALA2015092205779](https://openairdocs.org/sdr/DALA2015092205779.md): Retainer · cracked · Sep 20, 2015 · N908DL · Doug MD88 · Emergency Exits
  > CRACKED SEAL RETAINER AT RT FWD EMERGENCY DOOR LOWER AREA, REF NRC CARD 92, ZONE 201. SEAL RETAINER AT RT FWD EMERGENCY DOOR LOWER AREA, REF NRC CARD 92, ZONE 201 WAS REPLACED IAW SRM 51-30-2. CRACK LENGTH 0.437".
- [SDR DALA2015092105741](https://openairdocs.org/sdr/DALA2015092105741.md): Floor Panel · delaminated · Sep 20, 2015 · N908DL · Doug MD88 · Fuselage Floor Panel
  > ACFT HAS DELAMINATED FLOOR PANE. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.
- [SDR DALA2015092105740](https://openairdocs.org/sdr/DALA2015092105740.md): Floor Panel · corroded · Sep 20, 2015 · N908DL · Doug MD88 · Fuselage Floor Panel
  > CORRODED FLOOR PANEL. FLOOR PANEL FABRICATED AND REPLACED IAW AMM 53-20-01-201.
- [SDR DALA2015092105738](https://openairdocs.org/sdr/DALA2015092105738.md): Frame · corroded · Sep 20, 2015 · N908DL · Doug MD88 · Fuselage Main, Frame
  > ACFT HAS CORROSION ON PREVIOUS REPAIR TRIPLER ON FRAME ANGLE AT BS 1463 FROM LONGERONS 6 - 18L AT AFT ACCESSORY COMPARTMENT. REPAIR TRIPLER WAS REPLACED IAW SR J060287. REV AND SRM 51-30-5, 51-10-2 AND 53-03D, FIG 27, 51-10-3, PAR 21,14.
- [SDR DALA2015092105734](https://openairdocs.org/sdr/DALA2015092105734.md): Cargo Track · corroded · Sep 20, 2015 · N908DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT CARGO TRACK BS 1156 - 1322 AT AFT CARGO COMPARTMENT C3. TIE TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4, 51-10-3 PAR 21 AND 14, AND DOUGLAS DWG NR 5956705.
- [SDR DALA2015092105733](https://openairdocs.org/sdr/DALA2015092105733.md): Finger Doubler · cracked · Sep 20, 2015 · N908DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION AND CRACK ON SPLICE FINGER DOUBLER AT LONGERON 26, LT FROM BS 1251 - 1260 C3. CRACK DIMENTION IS 1.00" THE SECTION FINGER DOUBLER DAMAGE WAS REMOVED AND NEW SECTION WAS FABRICATED AND WAS TREATED AND PAINTED AND WAS INSTALLED IAW SRM 51-10-1, FIG 36
- [SDR DALA2015092005730](https://openairdocs.org/sdr/DALA2015092005730.md): Cargo Track · corroded · Sep 20, 2015 · N908DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > ACFT HAS CORROSION ON RT CARGO TRACK BS 1008-1322. THE CARGO TRACK WAS REPLACED IAW SRM 53-05, FIG 4C AND 51-30-2 AND 51-30-1, 51-10-4, 51-10-3 PAR 14 AND 21.
- [SDR DALA2015092105739](https://openairdocs.org/sdr/DALA2015092105739.md): Floor Panel · punctured · Sep 19, 2015 · N908DL · Doug MD88 · Fuselage Floor Panel
  > PUNCTURED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.
- [SDR DALA2015092005728](https://openairdocs.org/sdr/DALA2015092005728.md): Channel · cracked · Sep 19, 2015 · N908DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED AFT CHANNEL BS 994 X-53 AT RT WHEEL WELL. TEE WAS REPLACED IAW SRM 51-10-4 AND DWG 5936395, REV BF AND SRM 51-10-3, PAR 14, 21 ALSO SRM 51-30-2, 51-30-5A.
- [SDR DALA2015092005727](https://openairdocs.org/sdr/DALA2015092005727.md): Frame · cracked · Sep 19, 2015 · N908DL · Doug MD88 · Fuselage Main, Frame
  > ACFT HAS A CRACK ON PREVIOUS TRIPLER REPAIR ON FRAME ANGLE AT BS 1464 ON LONG 18R AT AFT ACCESSORY COMPARTMENT. TRIPLER REPAIR ON FRAME CLIP WAS REPLACED IAW SRM 51-10-4; 51-30-5 AND SR J060287-12, REV.
- [SDR DALA2015092005724](https://openairdocs.org/sdr/DALA2015092005724.md): Beam · corroded · Sep 19, 2015 · N908DL · Doug MD88 · Fuselage Main, Structure
  > ACFT HAS CPCP CORROSION ON BEAM FROM BS 639 - 691 AT CENTER LOWER CARGO COMP DOOR JAMB. SPACER WAS REPLACED IAW SRM 51-30-5 AND 53-05, FIG 123-A 51-10-3, PAR 14 AND 21, 38.
- [SDR DALA2015091805700](https://openairdocs.org/sdr/DALA2015091805700.md): Cusp Web · corroded · Sep 18, 2015 · N908DL · Doug MD88 · Fuselage Miscellaneous Structure
  > ACFT HAS CORROSION ON LT CUSP WEB BS Y= 670 TO 672 AND 696 TO 710 BETWEEN X=54 TO 60 AT PASSENGER CABIN FLOOR STRUCTURE. CORROSION WAS ATTENDED WITH SRM 51-30-2, 53-05 FIG. 131A-13, 51-10-3, PARA 14, 21, 38.

Next page: https://openairdocs.org/deregistered/N908DL-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 = 'N908DL' AND deregistration_id = 'N908DL-2022-11-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N908DL-2022-11-29/reports

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