# Service difficulty reports: Mcdonnell Douglas MD 83

A list on [Mcdonnell Douglas MD 83](https://openairdocs.org/model/mcdonnell-douglas-md-83.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 69 · 3,414 reports

- [SDR 2WAA2026FA0000318](https://openairdocs.org/sdr/2WAA2026FA0000318.md): Light · inoperative · May 1, 2026 · N802WA · Doug MD83 · Emergency Lighting
  > DURING PREFLIGHT INSPECTION, FLIGHT CREW REPORTED THAT THE TAIL CONE LIGHT WAS INOPERATIVE. ADDITIONALLY, WHEN THE EMERGENCY LIGHTING SYSTEM WAS ACTIVATED, MULTIPLE CEILING LIGHTS DID NOT ILLUMINATE AS REQUIRED. THE EMERGENCY EXIT LIGHT AT THE L2 DOOR WAS ALSO
- [SDR 2025F00277](https://openairdocs.org/sdr/2025F00277.md): Warning Light · illuminated · Dec 1, 2025 · N802W · Doug MD83 · Central Warning
  > TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ON, FLOW LIGHT ON DURING CLIMB AND UNABLE TO MAINTAIN PRESSURIZATION.
- [SDR 2WAA2025091000218](https://openairdocs.org/sdr/2WAA2025091000218.md): A/C Pack · no discrepancy · Sep 9, 2025 · N805WA · Doug MD83 · Cabin Cooling System
  > BURNING SMELL REPORTED AFTER FLIGHT BY FLT ATTENDANTS SUSPECTED FROM LEFT PACK PER THEM. PERFORMED INSPECTION WITH L/H AND R/H A/C PACKS AND NO DISCREPANCY FOUND AS PER MD80 AMM 21-00-00: PERFORMED INSPECTION LEFT AND RIGHT ELECTRIC SYSTEMS NO DISCREPANCY FOUN
- [SDR 2025F00212](https://openairdocs.org/sdr/2025F00212.md): Fire Warning · false activation · Sep 3, 2025 · N801WA · Doug MD83 · Fire Detection
  > 1.FWD CARGO FIRE INDICATION//2. FWD CARGO FIRE BOTTLE WAS DISCHARGE. AFTER REPLACING FIRE EXTINGUISHER COMPONENTS REF ITEM 2, OPS CHECK FOUND NORMAL IAW MD80AMM 26-18-02. 2. PERFORMED MAINTENANCE PROCEDURES FOLLOWING SYSTEM DISCHARGE. REPLACED COMPONENTS IAW M
- [SDR 2WAA20250820191](https://openairdocs.org/sdr/2WAA20250820191.md): Skin · corroded · Aug 20, 2025 · N808WA · Doug MD83 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AT UPPER CENTER EDGE AREA AND LOWER SECTION. REPAIRED RIGHT HORIZONTAL STABILIZER LEADING EDGE PER E.O.'S WAA-250319, WAA-250623, AND E.O. WAA-250620.
- [SDR 2WAA202508200190](https://openairdocs.org/sdr/2WAA202508200190.md): Skin · corroded · Aug 20, 2025 · N808WA · Doug MD83 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AT UPPER EDGE, ALL THRU THE LENGHT ALSO THE HARWARE OF LOWER EDGE IS RUSTY AND HAS CORROSION AROUND THE FASTENER HEAD. REPAIRED LEADING EDGE PER E.O.'S WAA-250220, WAA-250221, WAA-250222, WAA-250223, WAA-2
- [SDR 2WAA20250820192](https://openairdocs.org/sdr/2WAA20250820192.md): Window Frame · corroded · Aug 19, 2025 · N808WA · Doug MD83 · Fuselage Main, Structure
  > MAIN CABIN RIGHT SIDE WINDOW # 21 HAS CORROSION AROUND CUT OUT. ACCOMPLISHED REPAIR AT WINDOW # 21 R/H SIDE OF FUSELAGE BETWEEN BS 616 AND BS 636 PER E.O. WAA-250219
- [SDR 2WAA202508190186](https://openairdocs.org/sdr/2WAA202508190186.md): Window Frame · corroded · Aug 19, 2025 · N808WA · Doug MD83 · Fuselage Main, Structure
  > MAIN CABIN LEFT SIDE WINDOW CUT OUT HAS SEVERAL CORROSION 4, 5, 13, 29, 43, 51. ACCOMPLISHED CORROSION REMOVAL AT MAIN CABIN LEFT SIDE WINDOW CUT OUT NBR 4,13, 29, 43, 51, FOUND WITHIN LIMITS AND REPAIR WINDOW AT # 5 POSITION PER E.O. WAA-250227, MD-80 SRM 53
- [SDR 2WAA202508190183](https://openairdocs.org/sdr/2WAA202508190183.md): Angle · corroded · Aug 19, 2025 · N808WA · Doug MD83 · Fuselage Miscellaneous Structure
  > MAIN CABIN L/H SIDE LAVATORY HAS CORROSION ALL AROUND FLOOR BASE ATTACHMENT AREA. ACCOMPLISH L/H SIDE LAVATORY STRUCTURAL REPAIR IAW E.O. WAA 250403.
- [SDR 2WAA202508190182](https://openairdocs.org/sdr/2WAA202508190182.md): Angle · corroded · Aug 19, 2025 · N808WA · Doug MD83 · Fuselage Miscellaneous Structure
  > FWD LAVATORY L/H SIDE HAS CORROSION ALL AROUND THE FLOOR BASE. ACCOMPLISH FWD LAVATORY L/H SIDE STRUCTURAL REPAIR IAW E.O. WAA-250303
- [SDR 2WAA202508190181](https://openairdocs.org/sdr/2WAA202508190181.md): Angle · corroded · Aug 19, 2025 · N808WA · Doug MD83 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT R/H LAVATORY HAS CORROSION ALL AROUND THE FLOOR BASE AND INCORRECT HOSE INSTALL. ACCOMPLISHED AFT R/H LAVATORY STRUCTURAL REPAIR IAW E.O. WAA-250503.
- [SDR 2WAA202508190185](https://openairdocs.org/sdr/2WAA202508190185.md): Battery Pack · discharged · Aug 19, 2025 · N808WA · Doug MD83 · Emergency Lighting
  > MULTIPLES INTERNAL AND EXTERNAL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS AND EMERGENCY LIGHTSPER MD-80 AMM 33-53-00 OPS CKECK OK.
- [SDR 2WAA202508180189](https://openairdocs.org/sdr/2WAA202508180189.md): Skin · corroded · Aug 18, 2025 · N808WA · Doug MD83 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AT UPPER EDGE, ALL THRU THE LENGHT ALSO THE HARDWARE OF LOWER EDGE IS RUSTY AND HAS CORROSION AROUND THE FASTENER HEAD. REPAIR DONE BY E.O. WAA-250220, 250221, 250222, 250223, 25024, 250225, 250615.
- [SDR FXGA07302025001](https://openairdocs.org/sdr/FXGA07302025001.md): Duct · cracked · Jul 29, 2025 · N962CE · Doug MD83 · Engine Bleed Air System
  > TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED DURING CLIMB. FOUND RT BLEED AIR SOURCE DUCT WELD BROKEN. REMOVED AND REPLACED 13THSTAGE BLEED AIR SOURCE DUCTING BETWEEN ENGINE AND AUGMENTER VALVE IAW AMM 20-10-11. LEAK CHECK GOOD IAW AMM 71-00-00 CONFIG 4 STEP 4
- [SDR FXGA07292025002](https://openairdocs.org/sdr/FXGA07292025002.md): Overheat Sensor · activated · Jul 29, 2025 · N962CE · Doug MD83 · Engine Bleed Air System
  > TAIL COMPARTMENT TEMP HIGH ILLUMINATED, REPLACED R/H TAIL COMPARTMENT TEMP SENSOR IAW MD-80 AMM 36-20-02. OPERATIONAL CHECK GOOD
- [SDR FXGA07292025001](https://openairdocs.org/sdr/FXGA07292025001.md): Duct Clamp · leaking · Jul 29, 2025 · N962CE · Doug MD83 · Engine Bleed Air System
  > TAIL COMPARTMENT TEMP HIGH ILLUMINATED, FOUND #2 ENGINE BLEED AIR LEAK IN TAIL SECTION, REPLACED CLAMP IAW MD-80 AMM 20-10-11. GROUND RUN-UP OPERATIONAL CHECK GOOD.
- [SDR 2WAA2025070200158](https://openairdocs.org/sdr/2WAA2025070200158.md): Light · burned out · Jun 28, 2025 · N805WA · Doug MD83 · Emergency Lighting
  > LOW LEVEL EMERGENCY LIGHTS ON SEATS ROWS 21-32 BURNED OUT
- [SDR Y2PA2025061825006](https://openairdocs.org/sdr/Y2PA2025061825006.md): Skin Splice · corroded · Jun 18, 2025 · N831US · Doug MD83 · Wing, Plate/Skin
  > DISCREPANCY: WHILE AT C-CHECK IN KBQK, STAMBAUGH AVIATION FOUND CORROSION ON THE L/H WING LOWER SURFACE AT STR. 17 (SKIN SPLICE) AND AT XCW 85. BLENDED OUT THE DAMAGED AREA, PERFORMED HFEC OPEN HOLE INSPECTION AND FABRICATED A REPAIR DOUBLER USING 2024T3.12
- [SDR 2025F00137](https://openairdocs.org/sdr/2025F00137.md): Lamp · inoperative · May 30, 2025 · N801WA · Doug MD83 · Emergency Lighting
  > DURING DAILY CHECK FOUND SOME EMERGENCY FLOOR PATH LIGHT ARE NOT WORKING
- [SDR 2WAA20250401086](https://openairdocs.org/sdr/2WAA20250401086.md): Engine · failed · Mar 31, 2025 · N802WA · Doug MD83 · Engine (Turbine/Turboprop)
  > LH ENGINE FAILURE AFTER TAKEOFF
- [SDR 2WAA202503200067](https://openairdocs.org/sdr/2WAA202503200067.md): Valve · failed · Mar 19, 2025 · N805WA · Doug MD83 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF AND RISING LANDING GEAR, THE LANDING GEAR'S RED NOSE LIGHT WAS NOT EXTINGUISHED.
- [SDR 2025FA0000194](https://openairdocs.org/sdr/2025FA0000194.md): Battery Pack · discharged · Mar 15, 2025 · N805WA · Doug MD83 · Emergency Lighting
  > CABIN DISCREPANCY REPORT (CDR) ROW 3 AND SERVICING EMERGENCY LIGHTS NOT WORKING ROW 21, 23 ISLE PATH LIGHTING NOT WORKING EXIT LIGHT OF L1, R1 AND L2.
- [SDR 2025F00062](https://openairdocs.org/sdr/2025F00062.md): Skin · dented · Mar 12, 2025 · N805WA · Doug MD83 · Fuselage Main, Plate/Skin
  > THE L/H UPPER FUSELAGE BETWEEN STA-218 AND STA-237 HAS STRUCTURAL DAMAGE.
- [SDR 2WAA202502270051](https://openairdocs.org/sdr/2WAA202502270051.md): Light · inoperative · Feb 24, 2025 · N805WA · Doug MD83 · Emergency Lighting
  > EMERGENCY LIGHTS AT CABIN AFT DOOR INOP
- [SDR 2WAA202502270054](https://openairdocs.org/sdr/2WAA202502270054.md): Control Module · inoperative · Feb 24, 2025 · N805WA · Doug MD83 · Emergency Lighting
  > EMERGENCY LIGHTS AT INBOARD OVERWING EXIT DOORS L/H AND R/H ARE INOP
- [SDR 2WAA202502270052](https://openairdocs.org/sdr/2WAA202502270052.md): Battery Pack · discharged · Feb 24, 2025 · N805WA · Doug MD83 · Emergency Lighting
  > EMERGENCY LIGHTSAT L1 AND L2DOORS ARE INOP (NOT TESTING)
- [SDR 2025F00042](https://openairdocs.org/sdr/2025F00042.md): Control Module · failed · Feb 11, 2025 · N805WA · Doug MD83 · Emergency Lighting
  > EMERGENCY LIGHTS FWR EXIT LEFT AND RIGHT WERE FOUND VERY DIM. AFTER TROUBLESHOOTING THE MODULE CONTROL ASSY AB5-1 WAS REPLACED. THE OPERATIONAL TEST WAS FOUND NORMAL IAW MD-80 AMM 33-53-00.
- [SDR 2WAA20250205036](https://openairdocs.org/sdr/2WAA20250205036.md): Light · inoperative · Feb 5, 2025 · N805WA · Doug MD83 · Emergency Lighting
  > EMERGENCY EXIT LIGHT INOP
- [SDR 2024F00139](https://openairdocs.org/sdr/2024F00139.md): Clamp · loose · May 24, 2024 · N802WA · Doug MD83 · Cabin Pressure Control System
  > DURING CRUISE FLOW LIGHT ON AND DURING DESCENT CABIN ALTITUDE LIGHT ON, CABIN OXYGEN LIGHT ON, OXYGEN MASKS DEPLOYED. THE CORRECTIVE ACTION RESECURED CLAMPS OF A/C COMPONENTES AT AFTER PRESSURE BULKHEAD, FUNCTIONAL TEST OF CABIN PRESSURE CONTROL SYSTEM I.A.W
- [SDR 2024F00137](https://openairdocs.org/sdr/2024F00137.md): Battery · inoperative · May 20, 2024 · N805WA · Doug MD83 · Emergency Lighting
  > ON THE L1 DOOR JAMB THE EMERGENCY LIGHT LOCATED ON THE FRAME OF THE DOOR FAIL TEST PERFORMED DURING C-CHECK. REF. TASK CARD 53-200-05-01, WO 6549 CORRECTIVE ACION: REMOVED NAD REPLACE BATTERIES PACK L1 DOOR LAP EMERGENCY LIGHT I.A.W. MD80 AMM 33-53-00. PN: 10-
- [SDR FXGA20240426001](https://openairdocs.org/sdr/FXGA20240426001.md): Unlock Cylinder · leaking · Apr 25, 2024 · N962CE · Doug MD83 · Nose/Tail Landing Gear
  > NOSE LANDING GEAR FAILED TO EXTEND WITH NORMAL MEANS, CYCLED GEAR AND NOSE GEAR EXTENDED NORMALLY. LANDED WITH NO FURTHER INCEDENT
- [SDR FXGA20240417001](https://openairdocs.org/sdr/FXGA20240417001.md): Hinge · worn · Apr 16, 2024 · N963CE · Doug MD83 · Fuselage, Door Hinge
  > BIG VIBRATION FELT AFTER TAKEOFF IN AIRCRAFT AND YOKE. NOSE GEAR FORWARD DOORS CLOSING LINKAGE FOUND TO BE WORN
- [SDR 2024F00015](https://openairdocs.org/sdr/2024F00015.md): Oven · odor · Jan 22, 2024 · N802WA · Doug MD83 · Buffet/Galleys
  > CREW DISCREPANCY REPORT (CDR) #1 FWD CABIN GALLEY OVEN SMELL OF BURNED PLASTIC WHEN IN USE (LEFT SIDE) LP27780. OEM: BUDERUS SELL GMBH GERMANY
- [SDR 2023F00218](https://openairdocs.org/sdr/2023F00218.md): Window · detached · Jun 29, 2023 · N808WA · Doug MD83 · Passenger Compartment Windows
  > DURING A CRUISE AT FL 300, THE FLIGHT MECHANIC REPORTED TO THE FIRST OFFICER AND CAPTAIN THAT A PASSENGER WINDOW WAS BLOWN OUT. THE FIRST OFFICER CHECKED THE PRESSURIZATION WHICH WAS STABILIZED AND INDICATED NORMAL. THE FIRST OFFICER ASKED FOR THE ROW LOCATION
- [SDR 2023FA0000306](https://openairdocs.org/sdr/2023FA0000306.md): Unknown · unknown · Jun 8, 2023 · N965CE · Doug MD83 · Wing Structure
  > LEFT WINGTIP MADE CONTACT WITH AN ALUMINUM GATE. DAMAGE TO LEFT WINGTIP
- [SDR FXGA202301142301](https://openairdocs.org/sdr/FXGA202301142301.md): None · none · Jan 14, 2023 · N967CE · Doug MD83 · Fuselage Structure (General)
  > MAIN CARGO DOOR AFT SEAL DEPRESSOR PERMANENT REPAIR REFERENCE AEI TICKET 21004 R00 (002) STEP 1.2. TO REPAIR DAMAGE TO MAIN CARGO DOOR AFT SEAL DEPRESSOR. CUTOUT EXISTING SEAL DEPRESSOR DAMAGES SECTION AT AEO PROPOSED CUTOUT LINES AS PER ATTACHED (967 MCD #3)
- [SDR FXGA202211172230](https://openairdocs.org/sdr/FXGA202211172230.md): None · none · Nov 17, 2022 · N967CE · Doug MD83 · Fuselage Structure (General)
  > FUSELAGE SKIN GOUGED AT F/STA 463, STR 21L. TO REPAIR A DEEP GOUGE ON FUSELAGE SKIN. PERFORM SKIN REPAIR PER AEI EO 20455.
- [SDR FXGA202211112229](https://openairdocs.org/sdr/FXGA202211112229.md): None · none · Nov 11, 2022 · N961CE · Doug MD83 · Empennage Structure
  > MAIN CARGO DOOR LATCHES REPAIR. DURING TORQUE TUBE ISSUES ON ABOVE AIRCRAFT, ALL LATCHES RESULTED WITH GOUGES CAUSED BY THE LOCK PINS. IN ORDER TO CONTINUE WITH LATCHES EVALUATION, IT WILL BE REQUIRED TO BLEND OUT THE LATCHES AND PROVIDE THE THICKNESS OF REM
- [SDR FXGA202210102224](https://openairdocs.org/sdr/FXGA202210102224.md): None · none · Oct 10, 2022 · N965CE · Doug MD83 · Fuselage Structure (General)
  > DENT ON FUESELAGE SKIN AT F/STA 393, STR 15L. TO REPAIR DENT DAMAGE ON THE FUSELAGE SKIN AT F/STA 393, STR 15L. PERFORM FUSELAGE SKIN REPAIR PER STS EA 81-2022-122. RE-INSPECTION INSTRUCTIONS TO BE PROVIDED WITH DTA NO LATER THAN 12 MONTHS FROM REPAIR COMPLETI
- [SDR Y2PA2022090622047](https://openairdocs.org/sdr/Y2PA2022090622047.md): Skin · corroded · Aug 30, 2022 · N831US · Doug MD83 · Fuselage Structure (General)
  > DISCREPANCY: DURING C-CHECK AT COMMERCIAL JET IN KDHN, CORROSION FOUND ON FUSELAGE SKIN INTERNAL DOUBLER AT DRAIN VALVE MOUNTING SURFACE AT STATION 157
- [SDR Y2PA2022090622046](https://openairdocs.org/sdr/Y2PA2022090622046.md): Flap · corroded · Aug 30, 2022 · N831US · Doug MD83 · Trailing Edge Flaps
  > DISCREPANCY:: DURING C-CHECK AT COMMERCIAL JET IN KDHN, EXFOLIATION CORROSION FOUND ON RH WING INBOARD FLAP AT APPROXIMATELY XRS 69 INNER SURFACE EMANATING FROM UNDER RIB JUST BELOW 3RD FROM INBOARD FLAP VANE MOUNT
- [SDR Y2PA2022090622045](https://openairdocs.org/sdr/Y2PA2022090622045.md): Latch · cracked · Aug 30, 2022 · N831US · Doug MD83 · Cargo/Baggage Doors
  > DISCREPANCY: DURING C-CHECK AT COMMERCIAL JET IN KDHN, THE MAIN CARGO DOOR LATCH BASE LUG FITTINGS 3,4,5,6 AND 7 WERE FOUND TO BE CRACKED AT FASTENER HOLES DURING THE ACCOMPLISHMENT OF AD 2004-11-07 (PSE 52.80.FC3) HFEC INSPECTION OF THE MAIN CARGO DOOR LATCH
- [SDR FXGA202206212218](https://openairdocs.org/sdr/FXGA202206212218.md): Retainer · damaged · Jun 21, 2022 · N961CE · Doug MD83 · Doors
  > SEAL RETAINER INSTALLATION - DEVIATION. DAMAGED SEAL RETAINER PN: AE5660-11 MUST BE REPLACED WITH ALTERNATE PN: AE5738-16. DURING A VISUAL INSPECTION AROUND THE DOOR, IT WAS FOUND A CRACKED SEAL RETAINER PN: AE5660-11 (SEE FIGURE 1). THUS, A SECTION OF EXISTIN
- [SDR FXGA202205252213](https://openairdocs.org/sdr/FXGA202205252213.md): Longeron Splice · corroded · May 25, 2022 · N964CE · Doug MD83 · Fuselage Structure (General)
  > CORRODED LONGERON AND SPLICES FROM F/STA 1211 TO 1259. TO REMOVE AND REPLACE A CORRODED LONGERON SECTION (29L) AND ITS TWO CORRODED SPLICES AT F/STA 1211 AND 1259. REMOVED CORRODED SPLICES AND STRINGER SECTION, REPLACE WITH NEW. PERFORM ALL WORK FROM DC-9/MD-
- [SDR FXGA202112282139](https://openairdocs.org/sdr/FXGA202112282139.md): None · none · Dec 28, 2021 · Doug MD83 · Fuselage Structure (General)
  > FUSELAGE SKIN DAMAGED AT CANT STA 1497. TO REPAIR A DENT IN THE FUSELAGE SKIN AT CANT STATION 1497. FUSELAGE SKIN @ CANT/STA 1497 R/H DAMAGED. SEE ATTACHED REPORT NO. NR-0155SA REV IR FOR ACCOMPLISHMENT INSTRUCTION AND 8110-3 APPROVAL.
- [SDR FXGA2021102001](https://openairdocs.org/sdr/FXGA2021102001.md): None · none · Nov 2, 2021 · N962CE · Doug MD83 · Air Distribution System
  > LEFT PAC SUPPLY PRESSURE DROPPED TO ZERO FOLLOWED BY LOSS OF PRESSURIZATION WHILE IN CRUISE TO ANC. FOUND LOOSE CLAMP AND DUCTING FROM ACM OUTPUT.
- [SDR FXGA20210721001](https://openairdocs.org/sdr/FXGA20210721001.md): Pump · faulted · Jul 16, 2021 · N964CE · Doug MD83 · Fuel Boost Pump
  > CENTER FUEL PRESSURE LOW LIGHT ILLUMINATED/CENTER TANK FAILS TO FEED IN FLIGHT. RAN QRH PROCEDURE.(FOUND AFT CENTER FUEL TANK BOOST PUMP CIRCUIT BREAKER OPEN)
- [SDR FXGA20210328](https://openairdocs.org/sdr/FXGA20210328.md): Fire Detector · false activation · Mar 26, 2021 · N965CE · Doug MD83 · Fire Detection
  > CARGO FIRE MASTER WARNING ILLUMINATED WITH LOWER AFT COMPARTMENT FIRE INDICATION. NO FIRE DETECTED AFTER LANDING.
- [SDR 2WAA202104220084](https://openairdocs.org/sdr/2WAA202104220084.md): Instrument Panel · multiple fail · Mar 22, 2021 · N806WA · Doug MD83 · Independent Instruments
  > DURING ADVERSE WEATHER LOST MULTIPLE NAV GUIDANCE INSTRUMENTS, AUTO THROTLE AND AUTO PILOT, DECLARED EMERGENCY DIVERTED TO KIAH. UPON LANDING EVERTHING RETORNED TO NORMAL.
- [SDR FXGA20201026](https://openairdocs.org/sdr/FXGA20201026.md): Control Cable · binding · Oct 26, 2020 · N967CE · Doug MD83 · Landing Gear Retraction/Extension System
  > GEAR HANDLE STUCK IN UP POSITION, UNABLE TO LOWER THE GEAR IN BET ON FINAL APPROACH RWY 19. RETURN TO ANC, UNABLE TO LOWER THE FLAPS IN LANDING IN ANC, UNTIL 5 MILE FINAL, THEN THEY STARTED WORKING AGAIN. DECLARED EMERGENCY IN ANC PERFORMED EMERGENCY GEAR E

Next page: https://openairdocs.org/model/mcdonnell-douglas-md-83/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 aircraft_model_key = 'MD83'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/mcdonnell-douglas-md-83/reports

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