# Service difficulty reports: N908DE, cancelled Nov 8, 2022

A list on [N908DE, cancelled Nov 8, 2022](https://openairdocs.org/deregistered/N908DE-2022-11-08.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 · 174 reports

- [SDR DALA2020042002276](https://openairdocs.org/sdr/DALA2020042002276.md): Unknown · malfunctioned · Apr 19, 2020 · N908DE · Doug MD88 · Emergency Lighting
  > THE CABIN EMERGENCY LIGHTS ARE FLICKERING ON AND OFF WITH THE COCKPIT SWITCH IN THE ARMED POSITION WHILE IN FLIGHT. MAINTENANCE CYCLED THE CABIN EMERGENCY LIGHTS FROM THE CABIN AND COCKPIT POSITIONS NUMEROUS TIMES AND MONITORED THE LIGHTS FOR ANY FLICKERING. N
- [SDR DALA2020030301547](https://openairdocs.org/sdr/DALA2020030301547.md): Light · intermittent · Mar 2, 2020 · N908DE · Doug MD88 · Emergency Lighting
  > CABIN EMERG LIGHTS FLICKERING IN FLIGHT AND ON TAXI IN. NO COCKPIT INDICATIONS. ARMED EMERGENCY LIGHTS MONITORED EMERGENCY LIGHTS COULD NOT DUPLICATE FAULT. OK FOR SVC. (LP6993397)
- [SDR DALA2020022201336](https://openairdocs.org/sdr/DALA2020022201336.md): Longeron · cracked · Feb 21, 2020 · N908DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > REF: AMDS WC # 5314-2214, PSE/SSI # 53.80.003 WHILE ACCOMPLISHING LFEC INSPECTION, STEP (1), CRACK INDICATION IN LONGERON 2R NOTED AT THREE EACH FASTENERS, BETWEEN FS STA 886- 875 JUST FORWARD OF UPPER ANTI-COLLISION LIGHT. SEE NR FOR ADDITIONAL INFORMATION 00
- [SDR DALA2020020500891](https://openairdocs.org/sdr/DALA2020020500891.md): Light · malfunctioned · Feb 5, 2020 · N908DE · Doug MD88 · Emergency Lighting
  > FIRST CLASS EMERG LIGHTING FLASHING ON AND OFF / INTERIOR. PERF EMR LIGHTS TEST, ALL LIGHT TEST NML AT THIS TIME. NO FLASHING LIGHTS NOTED. (LP1476076)
- [SDR DALA2020011200204](https://openairdocs.org/sdr/DALA2020011200204.md): Light · malfunctioned · Jan 12, 2020 · N908DE · Doug MD88 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:602 / ACARS TEXT: FRC335201602 EMERG LIGHTS FIRST CLASS CABIN COME ON INT FOR ABOUT 10 SECONDS THEN TURN OFF / INTERIOR. PULLED AND RESET C/B Z37 AND A14.TESTED EMERGENCY LTS PER AMM 33-53.OPS CHECK N
- [SDR DALA2019091305295](https://openairdocs.org/sdr/DALA2019091305295.md): Unknown · malfunctioned · Sep 12, 2019 · N908DE · Doug MD88 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. EMERGENCY FLOOR LIGHTING DAMAGED OR INOP. TRACK LIGHTING GOES ON & OFF. CHECKED OPERATION OF EMERGENCY LIGHTS - UNABLE TO DUPLICATE PROBLEM - SYSTEM OP'S NORMAL REF AMM 33-53. (LP1267573)
- [SDR DALA2019090205111](https://openairdocs.org/sdr/DALA2019090205111.md): Wire · pulled · Sep 2, 2019 · N908DE · Doug MD88 · Light System Wiring
  > FA REPORTS DURING TAKEOFF EMERGENCY LIGHTS WERE FLASHING. COCKPIT SW. IN ARM FA SW. OFF. FA LATER REPORTED EMERGENCY LIGHTS ON BUT VERY DIM. FOUND WIRES PULLED OUT OF CONNECTOR AT SEAT 26E. REPLACED SEAT EMERGENCY LIGHT EXTENSION HARNESS. ALL CKS GOOD PER WDM
- [SDR DALA2019081324739](https://openairdocs.org/sdr/DALA2019081324739.md): Light · damaged · Aug 4, 2019 · N908DE · Doug MD88 · Exterior Lighting
  > RT TAXI LIGHT MISSING. FOUND BLUE RING TERMINAL FOR RT TAXI NOSE LIGHT DAMAGED. REMOVED AND REPLACED IAW SWPM CH.20. REPLACED MISSING RT NOSE LIGHT PER MD88 AMM 33-41.
- [SDR DALA2019070103936](https://openairdocs.org/sdr/DALA2019070103936.md): Smoke Detector · faulty · Jun 28, 2019 · N908DE · Doug MD88 · Smoke Detection
  > FIRST CLASS LAV SMOKE DETECTOR BEEPING. R/R FWD LAV SMOKE DETECTOR PER MD88 AMM 23-16. (LP1144630)
- [SDR DALA2019062403761](https://openairdocs.org/sdr/DALA2019062403761.md): Battery Pack · inoperative · Jun 24, 2019 · N908DE · Doug MD88 · Emergency Lighting
  > BOTH FWD OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERIES AT POWER SUPPLY B5-103. PREFORMED OPS CHECK IAW AMM 33-53. CHECKED OK. OK FOR SERVICE.
- [SDR DALA201906032358](https://openairdocs.org/sdr/DALA201906032358.md): Smoke Detector · malfunctioned · Jun 1, 2019 · N908DE · Doug MD88 · Smoke Detection
  > AIRCRAFT LEFT AFT LAV SMOKE DETECTOR IS CHIRPING. REMOVED & REPLACED AFT LEFT LAV SMOKE DETECTOR. OPS CHK GOOD. (LP1102304)
- [SDR DALA2019052903281](https://openairdocs.org/sdr/DALA2019052903281.md): Terminal · out of position · May 28, 2019 · N908DE · Doug MD88 · Emergency Lighting
  > FA REPORTS THAT EMERGENCY LIGHTS FLICKERS ON/OFF AT HALF BRIGHTNESS AT 3-4 MINUTE INTERVALS IN FLIGHT. FOUND OVERHEAD EMERGENCY LIGHT SWITCH TERMINAL TOUCH ADJACENT STRUCTURE. REPOSITION TERMINAL. PER WDM 33-51. REF SWPM CH 20. CKS GOOD. (LP5564892)
- [SDR DALA2019052103112](https://openairdocs.org/sdr/DALA2019052103112.md): Access Panel · missing · May 20, 2019 · N908DE · Doug MD88 · Engine Cowling System
  > FOUND ON ARRIVAL #1 ENG UPPER COWLING MISSING ACCESS PANEL. I/B SIDE JUST AFT OF NOSE COWL. INSTALLED #1 ENG INBD PANEL. (LP5564856)
- [SDR DALA2019042982690](https://openairdocs.org/sdr/DALA2019042982690.md): Engine · failed · Apr 26, 2019 · N908DE · Doug MD88 · Engine (Turbine/Turboprop)
  > ON SHORT FINAL HEARD A LOUD BANG FOLLOWED BY NOTICEABLE YAW MOMENT TO THE LEFT. LEFT ENGINE INSTRUMENTS ROLLED BACK TO 1.02 EPR 20 PERCENT N1 EGT 525, N2 48 PERCENT WITH THROTTLE @ APROX 1.3 ENGINE UNRESPONSIVE TO THROTTLE MOVEMENT ON GROUND. REMOVED AND REPLA
- [SDR DALA2019032601913](https://openairdocs.org/sdr/DALA2019032601913.md): Oven · malfunctioned · Mar 25, 2019 · N908DE · Doug MD88 · Buffet/Galleys
  > SHIP 9008 - ATB - RETURNED TO ATL DUE TO SMOKE DETECTOR IN FORWARD LAVATORY ACTIVATED ALONG WITH STRONG SMELL ON TAKE-OFF AT 300FT. CORRECTIVE ACTION: WHILE WORKING NO GO ODI WORK CARD 2120-2367 FOUND OVEN PRODUCING ODOR DESCRIBED ON SMOKE AND FUMES QUESTIONNA
- [SDR DALA2019020400701](https://openairdocs.org/sdr/DALA2019020400701.md): Slide · damaged · Feb 3, 2019 · N908DE · Doug MD88 · Escape Slide
  > 1L DOOR SLIDE LACING PINS UNDONE. REMOVE AND INSTALL L1 SLIDE PER WC 2561-4964 SLIDE, PASSENGE OFF 09-2561-9-0011 01919 ON 97-2561-9-0003 02652. (LP4752842)
- [SDR DALA2018102906327](https://openairdocs.org/sdr/DALA2018102906327.md): Floor Panel · damaged · Oct 27, 2018 · N908DE · Doug MD88 · Fuselage Floor Panel
  > CENTER AISLE FLOOR PANEL EXCESSIVE SPONGY AT ROW 24 WITH EDGE COVER FRACTURED. FOUND HARDWARE LOOSE RT SIDE FILLER PANEL. RESECURED. REPAIRED FILLER PANEL PER SRM 53-22. (LP5159970)
- [SDR DALA2018090405393](https://openairdocs.org/sdr/DALA2018090405393.md): Skin · cracked · Aug 31, 2018 · N908DE · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > WHILE IN C CHECK, ACCOMPLISHING REPETITIVE INSPECTIONS PER AD 2011-15-01 AND SB MD8880-55A067, MTC FOUND A CRACK COMMON TO A HOLE COMMON TO THE DORSAL SKIN, BELOW THE SKIN SPLICE AND IN THE INTERNAL OEM DOUBLER( P/N 9911960-3)ONLY, LOCATED APPROXIMATELY 15 FAS
- [SDR DALA2018083005358](https://openairdocs.org/sdr/DALA2018083005358.md): Skin · corroded · Aug 29, 2018 · N908DE · Doug MD88 · Fuselage Main, Plate/Skin
  > AFT LAVATORY SERVICE PANEL LOWER FUSELAGE SKIN WAS CORRODED. COMPLIED WITH PRI 570970-14, REV O.
- [SDR DALA2018082905338](https://openairdocs.org/sdr/DALA2018082905338.md): Torsion Bar · corroded · Aug 29, 2018 · N908DE · Doug MD88 · Spoilers
  > LEFT WING, CENTER SPOILER TORSION BAR CORRODED. REPLACED THE TORSION BAR IAW AMM 27-61-06.
- [SDR DALA2018082905337](https://openairdocs.org/sdr/DALA2018082905337.md): Torsion Bar · corroded · Aug 29, 2018 · N908DE · Doug MD88 · Spoilers
  > RT WING, MID SPOILER TORSION BAR CORRODED. REPLACED THE TORSION BAR IAW AMM 27-61-06.
- [SDR DALA2018082905336](https://openairdocs.org/sdr/DALA2018082905336.md): Torsion Bar · corroded · Aug 29, 2018 · N908DE · Doug MD88 · Spoilers
  > LEFT WING OTBD FLIGHT SPOILER TORSION BAR WAS CORRODED. REPLACED THE TORSION BAR IAW AMM 27-61-06.
- [SDR DALA2018082875307](https://openairdocs.org/sdr/DALA2018082875307.md): Skin · corroded · Aug 27, 2018 · N908DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION LOCATED AT THE AFT LAV SERVICE PANEL CUTOUT, BS 1307 - 1322, LONGERON 21L AND 22L.
- [SDR DALA2018062304166](https://openairdocs.org/sdr/DALA2018062304166.md): Linkage · obstructed · Jun 21, 2018 · N908DE · Doug MD88 · Power Lever
  > RT THROTTLE IS JAMMED AND STUCK AT IDLE POSITION. T/S REF AMM 76-11 THROTTLE OPERATION NML AFTER CARGO COMP 3 BAGS REMOVED FROM CEILING AREA INSP LINKAGE NO DISCREPANCIES NOTED NO 30 DAY HISTORY.
- [SDR DALA2018050403053](https://openairdocs.org/sdr/DALA2018050403053.md): Battery · discharged · May 2, 2018 · N908DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT INOP ON CEILING PANELS ON ROW 21-26. FOUND BATTERY BAD IN BATTERY PACK IN BAG BIN 24E,D. REPLACED BATTERIES. LIGHTS WORK GOOD.
- [SDR DALA2018041002313](https://openairdocs.org/sdr/DALA2018041002313.md): Engine · power loss · Apr 9, 2018 · N908DE · Doug MD88 · Engine (Turbine/Turboprop)
  > CLIMBING THRU FL230 A LOUD BANG OCCURED AND A DROP IN POWER ON THE LEFT ENGINE WAS OBSERVED. RAN QRH 7.6 CONTACTED OCC AND MCC. RAN QRH 7.45 AND ELECTED TO LEAVE ENGINE RUNNING AT IDLE DUE TO NORMAL OIL PRESSURE AND LACK OF VIBRATION OR FURTHER ABNORMAL INDICA
- [SDR DALA2018040902306](https://openairdocs.org/sdr/DALA2018040902306.md): Support Angle · cracked · Apr 8, 2018 · N908DE · Doug MD88 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENGINE NOSE COWL LOWER AREA AFT VERTICLE SUPPORT ANGLE CRACKED AT THE 5:30 POSITION. REMOVED AND REPLACED IAW AMM 71-10.
- [SDR DALA2017123009007](https://openairdocs.org/sdr/DALA2017123009007.md): Seat · out of adjust · Dec 29, 2017 · N908DE · Doug MD88 · Passenger Compartment Equipment
  > SEAT BACK LOOSE IMPEDES EXIT ROW BEHIND. ADJUSTED SEAT BACK FASTENERS IAW AMM 25-21, ACFT OK FOR SERVICE.
- [SDR DALA2017082506379](https://openairdocs.org/sdr/DALA2017082506379.md): Wire Harness · defective · Aug 25, 2017 · N908DE · Doug MD88 · Light System Wiring
  > DURING SERVICE CHECK FOUND EMERGENCY EXIT ROW 25DE SEAT PATH LIGHTING INOP. REPLACED HARNESS FROM WALL TO LIGHTS. OPS CHECK GOOD REF MD88 AMM 33-53. (LP3520720)
- [SDR DALA2017032902527](https://openairdocs.org/sdr/DALA2017032902527.md): Skin · cracked · Mar 28, 2017 · N908DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING A WALK AROUND, FOUND CRACKING IN SKIN IN 48 SECTION LOWER RIGHT SIDE UNPRESSURIZED AREA ABOVE ACCUM ACCESS DOOR. STOP DRILLED THE CRACK. FABRICATED A DOUBLER. TREATED, INSTALLED, AND PAINTED IAW SRM 53-01, PAGE 12, FIG 2, SHEET 3.
- [SDR DALA2017022801612](https://openairdocs.org/sdr/DALA2017022801612.md): Cable · frayed · Feb 27, 2017 · N908DE · Doug MD88 · Aerodynamic Fairings
  > TAILCONE CABLE FRAYED. REPLACED THE CABLE IAW AMM 53-53-00.
- [SDR DALA2016081105931](https://openairdocs.org/sdr/DALA2016081105931.md): Pin · missing · Aug 10, 2016 · N908DE · Doug MD88 · Escape Slide
  > MISSING LOCK PIN ON L1 AND L2 DOOR SLIDE. PINS INSTALLED IAW AMM 25-62-00.
- [SDR DALA2016081105930](https://openairdocs.org/sdr/DALA2016081105930.md): Cable · damaged · Aug 10, 2016 · N908DE · Doug MD88 · Hydraulic Power System Wiring
  > LOOSE LACING ON ELECTRICAL CABLE AT AUXILIARY HYDRAULIC PUMP AT RT MLG WW. LACING INSTALLED IAW ER/A 467688-14MA AD.
- [SDR DALA2016081105927](https://openairdocs.org/sdr/DALA2016081105927.md): Pin · misinstalled · Aug 10, 2016 · N908DE · Doug MD88 · Escape Slide
  > DURING OK TO INSTALL FWD SERVICE DOOR SLIDE, LOWER LOCK PIN WAS FOUNDED IMPROPERLY INSTALLED. FWD SERVICE DOOR SLIDE WAS REMOVED AND INSTALLED IAW AMM 25-62-00.
- [SDR DALA2016081005915](https://openairdocs.org/sdr/DALA2016081005915.md): Skin · cracked · Aug 9, 2016 · N908DE · Doug MD88 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND, 0.125 INCH IN LENGTH ON FUSELAGE SKIN BETWEEN BS 1418, LONGERON 2-3R. REPAIRED IAW ER/A 549225-14AD REV. ORIGINAL AND ETI-88-16-282.
- [SDR DALA2016080805857](https://openairdocs.org/sdr/DALA2016080805857.md): Frame · cracked · Aug 7, 2016 · N908DE · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1510. THE FRAME WAS REPLACED IAW 51-30-2 AND 51-30-5 AND DWG 9911843 REV. AC.
- [SDR DALA2016080605856](https://openairdocs.org/sdr/DALA2016080605856.md): Skin · damaged · Aug 5, 2016 · N908DE · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON OUTER FUSELAGE SKIN BS 170 BETWEEN LONGERONS 28 - 29L. REPAIRED IAW ETI 88-16-228 AND ER/A 547886-14 REV ORIGINAL.
- [SDR DALA2016080605855](https://openairdocs.org/sdr/DALA2016080605855.md): Skin · corroded · Aug 5, 2016 · N908DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON RT WING LOWER SKIN XRS 115. FAIRING WAS REMOVED, AREA WAS BLENDED, MEASURE (UT) NDT SPM 04-00-07 PAR 5 FIGURE 3 SHEET 1 & 2 WAS ACCOMPLISHED WITH ORIGINAL.340" MINIMUM REMAINING.333" AND FOUND WITHIN LIMITS, FLAP PENNING WAS PERFORMED, TREATED
- [SDR DALA2016080505786](https://openairdocs.org/sdr/DALA2016080505786.md): Beam · cracked · Aug 4, 2016 · N908DE · Doug MD88 · Passenger/Crew Doors
  > CRACKED BEAM NR 1 ON FWD ENTRY DOOR. PASSENGER FORWARD ENTRY DOOR WAS REMOVED AND INSTALLED IAW AMM 52-11-00 401. REPAIR BEAM NR 1 IAW SRM 52-05, FIG 98, SHEET 3.
- [SDR DALA2016080505785](https://openairdocs.org/sdr/DALA2016080505785.md): Frame · corroded · Aug 4, 2016 · N908DE · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME STA Y=1380, BETWEEN LONGERONS 29L-27R AT AFT ACCESSORY COMPARTMENT. FRAME WAS R & R IAW DWG 9912246-115, SRM 51-30-2, SRM 51-30-5 AND ER/A 547884-14, REV ORIGINAL.
- [SDR DALA2016080305726](https://openairdocs.org/sdr/DALA2016080305726.md): Skin · cracked · Aug 2, 2016 · N908DE · Doug MD88 · Horizontal Stabilizer, Plate/Skin
  > .405 INCH CRACK ON HORIZONTAL STABILIZER SKIN UPPER PANEL RT SIDE NEAR TO REAR SPAR PLANE BETWEEN XH=7.234 TO XH= 13.486. THE SKIN WAS REPLACED AND REPAIRED PER DWG SR09550028 REV.D AND SRM 51-30-2, SRM 51-30-5, SRM 51-30-9, SRM 51-10-3 PAR 14.21.
- [SDR DALA2016080305725](https://openairdocs.org/sdr/DALA2016080305725.md): Frame · cracked · Aug 2, 2016 · N908DE · Doug MD88 · Fuselage Main, Frame
  > CRACKED LOWER CAP ON FRAME BS 1437, LONGERON 2R. THE FRAME WAS REPAIRED IAW SRM 53-01 FIG. 2 & DWG 9953016 REV. AT.
- [SDR DALA2016080105705](https://openairdocs.org/sdr/DALA2016080105705.md): Bracket · cracked · Jul 31, 2016 · N908DE · Doug MD88 · Horizontal Stabilizer Structure
  > CRACKED RT HORIZONTAL STAB SIDE ROLLER BRACKET. THE ROLLER BRACKET WAS REPLACED AND ADJUSTED IAW AMM 55-10-00.
- [SDR DALA2016080105701](https://openairdocs.org/sdr/DALA2016080105701.md): Longeron · cracked · Jul 31, 2016 · N908DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 3L BS 1437. LONGERON REPAIRED IAW SRM 53-02 FIG. 18.
- [SDR DALA2016073105664](https://openairdocs.org/sdr/DALA2016073105664.md): Doubler · corroded · Jul 31, 2016 · N908DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER PRODUCTION DOUBLER BETWEEN BS 1222 - 1234 AND BS 1205 - 1216, LONGERONS 25 - 26L. THE DOUBLER WAS REPLACED IAW SRM 53-34-0 FIG 3 AND 51-10-1 FIG G.36 (SHEET 6).
- [SDR DALA2016080105704](https://openairdocs.org/sdr/DALA2016080105704.md): Splice · cracked · Jul 30, 2016 · N908DE · Doug MD88 · Wing Main, Frame Structure
  > CRACKED SPLICE ON FIXED LEADING EDGE STRUCTURE XFS=194.850 ON RT WING. THE DOUBLER WAS REPLACED IAW ER/A 379404-14MA REV.A.
- [SDR DALA2016073105663](https://openairdocs.org/sdr/DALA2016073105663.md): Cusp Web · corroded · Jul 30, 2016 · N908DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON PREVIOUS REPAIR DOUBLER OF LT CUSP WEB BETWEEN BS 1174 - 1193 AND X 54 - 60. THE DOUBLER WAS REPLACED IAW SRM 53-05 FIG 131A-7, SRM 51-30-5, AND SRM 51-10-3.
- [SDR DALA2016080105691](https://openairdocs.org/sdr/DALA2016080105691.md): Intercostal · cracked · Jul 29, 2016 · N908DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL X=0 BETWEEN STA Y=1041 TO Y=1022,Y=769 TO Y=788 AND Y=1287 TO Y=1307 ALSO X=4, STA Y=1287 TO Y=1271 AT FLOOR STRUCTURE CABIN. REPLACED INTERCOSTAL STA=1287 TO STA=1271 INTERCOSTAL STA=769 TO STA=788 WAS REPAIRED. 2 CRACKS 1-.250 AND 2-.
- [SDR DALA2016080105690](https://openairdocs.org/sdr/DALA2016080105690.md): Frame · cracked · Jul 29, 2016 · N908DE · Doug MD88 · Fuselage Main, Frame
  > CRACKS ON FRAME Y=1452 BETWEEN LONGERONS 1, 8L-9L AT AFT ACCESSORY COMPARTMENT. FRAME WAS REPLACED IAW DWG 9911860, REV L AND SRM 51-30-2,51-30-5 AND 51-10-3.
- [SDR DALA2016073105659](https://openairdocs.org/sdr/DALA2016073105659.md): Skin · cracked · Jul 29, 2016 · N908DE · Doug MD88 · Fuselage Main, Plate/Skin
  > .250 INCH CRACK IN FUSELAGE SKIN BS 1380 BETWEEN LONGERONS 12 - 13L. REPAIRED IAW SRM 53-04 FIG18 SHEET 1,2 AND 53-01 FIG 4 SHEET 4.

Next page: https://openairdocs.org/deregistered/N908DE-2022-11-08/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 = 'N908DE' AND deregistration_id = 'N908DE-2022-11-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N908DE-2022-11-08/reports

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