Boeing MD-90-30

Service difficulty reports · 6,066

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'MD9030'
  ORDER BY difficulty_date DESC"

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SDR DALA2020021001034Window Frame · crackedCRACK ON FRAME OF CLEAR VIEW WINDOW RH, UPPER AFT CORNER. (CPIL) INTERNAL DOUBLER WAS REPLACED PER DWG: 5911356 REV DJ, MD90 SRM 51-30-01, SRM 51-30-02 AND SRM 51-30-05 VOL. II. (1482734)Feb 9, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020021091036Floor Panel · damagedPANELS 222BF, 222LG,222UF WITH A MEASURE HIGTHER TO 20 PERCENT OF ALLOWED DAMAGE , THEREFORE THEY ARE OUT OF LIMITS PER MD-90 SRM VOL.1. 53-20-03 PARAGRAPH 5 FIGURE 2 FABRICATED, REPLACED AND IDENTIFIED PER MD-90 SRM VOL.I 53-20-03 PARAGRAPH 5 AND MUST BE INSTFeb 8, 2020 · N908DA · Doug MD9030 · Fuselage Floor PanelSDR DALA2020021081035Door Frame · corrodedCORROSION DOOR JAMB WEB ON STA 200-210 AND X =54 AT FWD WET AREA MRB 53?211?01 (W1) . CORROSION LEVEL 2. DOOR JAMB WEB ON STA 200-210 AND X=54 AT FWD WAS REPAIR PER MD-90 SRM 53-00-01 PAR.8 FIG.6 VOL.I (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR . 5 FIG 3 SFeb 8, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020021091033Floor Panel · delaminatedDURING INSPECTION BY DELAMINATION, WERE FOUND FLOOR PANELS 221BF, 221HF, 221JF AND 221LF ARE OUT OF LIMITS IN REF TO NRC 00406.(CPAX) FLOOR PANELS 221BF, 221HF, 221JF AND 221LF WERE FABRICATED REPLACED AND IDENTIFIED PER.MD-90. VOL.1 SRM 53-20- 03 FLOOR PANELSFeb 8, 2020 · N908DA · Doug MD9030 · Fuselage Floor PanelSDR DALA2020021091032Pan · crackedCRACKED OUTER PAN OVER BEAM # 5 STA 750 AT MID CARGO COMPARTMENT DOOR (PTAS) OUTER PAN OVER BEAM # 5 STA 750 AT MID CARGO COMPARTMENT DOOR WAS REPAIRED PER MD-90 SRM VOL. I 52-30- 02 PAR. 6 FIG. 4 (1481765)Feb 8, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020021091031Cusp Web · corrodedCORROSION ON LH CUSP WEB STA 256-274, 274- 293 AND 293-313 BTW X=54 AND X=60 MRB 53-211-01 (CPAX) SUMMARY OF NRC 00265: (CORROSION LEVEL 2) NEW CUSP WEB WAS INSTALLED PER MD-90 SRM 51-30-02. VOL II AND SRM 51-30-01 TOOLS USED : TORQUE WRENCH P/N 1501MRMH, S/N Feb 8, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020021081030Cusp Web · corrodedCORROSION ON LH CUSP WEB STA 670-674, 674- 693, 693-712, 712-731, 731-750, 750-769 BTW X=54 AND X=60 MRB 53 ?211?01 (CPAX) CORROSION LEVEL 2, CUSP WEB ON STA= 655 TO STA =769 WAS REPLACED PER MD-90 SRM VOL II 51-30-02 AND DWG 9930538-9 REV: CF (1481194)Feb 8, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020021081029Skin · crackedINITIAL INSPECTION: CRACK ON OUTER SKIN ABOVE HANDLE HOUSING AT FWD ENTRANCE DOOR (L1)(PTAS) ENTRANCE DOOR WAS REPAIRED PER ER/A 501106-14MA REVISION "C" ASSOCIATED ER/A 00-501106 ADDED FOR AC 9208 (1480715)Feb 8, 2020 · N908DA · Doug MD9030 · Passenger/Crew DoorsSDR DALA2020021001028Floorbeam · corrodedCORROSION ON FLOOR SUPPORT STA 522 BTW LONGS 26RH TO 26LH AT FWD CARGO COMPARTMENT MRB 53-302-07 (CCD) CORROSION LEVEL 1. CORROSION WAS REMOVED PER MD-90 SRM 51-10-03 PAR 26 (A) VOL II. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON FLOOR SUPPORT STA 522 BTW LONGS 2Feb 8, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020020500886Service Panel · corrodedCORROSION ON LAVATORY SERVICE PANEL (FUS) ( AMDS 5300-2264) SUMMARY OF NRC 00033. CORROSION LEVEL 2: LAVATORY SERVICE PANEL WAS REPLACED PER MD-90 SRM 51-30-02 AND 51-30-05 VOL. II (1475820)Feb 4, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020020500885Cusp Web · corrodedCORROSION ON LH CUSP WEB STA 598-605, 610- 617, 617-625 AND 650-655 BTW X=54 AND X=60 MRB 53?211?01 (CPAX) SUMMARY OF NRC 00110. CORROSION LEVEL 2. LH CUSP WEB STA 598-655 , WAS REPLACED PER MD 90 SRM 51-30-02 VOL.II AND 51-30-01 VOL II (1475482)Feb 4, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020020500884Cusp Web · corrodedAWR IN REF NRC 0118, CORROSION ON RH CUSP WEB STA Y=525 AT PASSENGER COMPARTMENT MRB 53-211-01 ENTR 00983062 W SUMMARY OF NRC 01186, CORROSION LEVEL 2 ; RH CUSP WEB STA Y=525 AT PASSENGER COMPARTMENT WAS REPAIRED PER MD-90 VOL. I SRM 53-20 -02 FIG.16. (1475479Feb 4, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020020400877Web · corrodedINITIAL INSPECTION: SEVERAL CORROSION POINTS ON DIAPHRAGM FROM STA Y=120 TO Y=149 X=-40 TO X=40 IN REF AMDS 5300-2573. (CPIL) CORROSION WAS REMOVED STA Y=120 TO Y=149 X=-40 TO X=40 PER MD 90 VOL. II SRM 51-10-03 PAR.26 (A).(UT) WAS ACCOMPLISHED PER NDT SPM 04-Feb 3, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020020400876Cusp Web · crackedCRACKED LH CUSP WEB ON STA 1140 BTW X=54 AND X=60 (CPAX) CUSP WEB ON STA 1140 BTW X=54 AND X=60 LH WAS REPAIRED PER MD 90 SRM 53-20-02 PAR. 6 FIG. 6 VOL. I. (1473860)Feb 3, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020020300794Door Frame · crackedINITIAL INSPECTION: CRACK ON DOOR JAMB WEB STA 207, LONG 11 LH ( L1) CRACK ON DOOR JAMB WEB STA 207, LONG 11 LH WAS REPAIRED PER. MD-90 SRM 53-60-02 FIG. 15 VOL. I. (1472823)Feb 2, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020020300793Door Frame · crackedCRACK ON DOOR JAMB WEB STA 207, LONG 15 LH ( L1) CRACK ON DOOR JAMB WEB STA 207, LONG 15 LH WAS REPAIRED PER. MD-90 SRM 53-60-02 FIG. 15 VOL. I. (1472815)Feb 2, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020020300792Frame · wornWEAR ON RING PAN LOWER MID EDGE AT STA Y= 1050 RH SIDE. (CPAX) C/A NRC 00285:RING PAN LOWER MID EDGE AT STA Y= 1050 RH SIDE WAS REPLACED PER MD-90 SRM 51-30-02 AND 51-30-05 VOL. II (1472757)Feb 2, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020020100775Door Frame · corrodedCORROSION ON PREVIOUS REPAIR SPACER AT AFT CARGO COMPT LOWER DOOR JAMB STA 1211 TO 1268 MRB 53-123-02 CARGO COMPT LOWER DOOR JAMB STA 1211 TO 1268 WAS REPLACED PER MD90 VOL. L SRM 53-60-02 FIG. 9 (1469805)Jan 31, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020020131774Seat Track · crackedCRACK ON RH SEAT TRACK X=-54 BTW STA= 1045 AND 1050 PASSENGER CABIN C/A SEAT TRACK X=-54 BTW STA= 1045 AND 1050 WAS REPAIRED PER MD-90 SRM 53-40-01 VOL. I PAR. 6. (1469198)Jan 31, 2020 · N908DA · Doug MD9030 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020020130773Frame · crackedCRACK ON RING PAN UPPER FWD EDGE AT STA Y= 943 LH SIDE. (CPAX) RING PAN UPPER FWD EDGE AT STA Y= 943 LH WAS REPAIRED PER MD-90 SRM 56-20-02 VOL. I PAR. 3 FIG. 2 (1468779)Jan 30, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020012800636Frame · crackedINITIAL INSPECTION: CRACK ON RING PAN UPPER FWD EDGE AT STA Y= 1003 RH SIDE. (CPAX) . SUMMARY OF NRC 00283:RING PAN UPPER FWD EDGE AT STA Y= 1003 RH SIDE WAS REPAIRED PER MD90-SRM VOL I 56-20-02 PAR. 3 FIG. 2. (LP# 1463818)Jan 27, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020012870635Floorbeam · crackedINITIAL INSPECTION: CRACKED FLOOR SUPPOR ON STA 1003 BTW X=10 AT PAX CABIN AREA (CPAX). SUMMARY OF NRC S/N 00837: CRACKED FLOOR SUPPOR ON STA 1003 BTW X =10 AT PAX CABIN AREA (CPAX) WAS REPLACED PER MD-90 SRM 51-30-05 VOL.II. (LP# 1463142)Jan 27, 2020 · N908DA · Doug MD9030 · Fuselage Main, Floor BeamSDR DALA2020012870634Floorbeam · crackedINITIAL INSPECTION: CRACKED FLOOR SUPPOR ON STA 1022 BTW X=15 AT PAX CABIN AREA (CPAX). SUMMARY OF NRC S/N 00835: CRACKED FLOOR SUPPOR ON STA 1022 BTW X =15 AT PAX CABIN AREA (CPAX) WAS REPLACED PER MD-90 SRM 51-30-05 VOL.II. (LP# 1463137)Jan 27, 2020 · N908DA · Doug MD9030 · Fuselage Main, Floor BeamSDR DALA2020012700633Floorbeam · crackedINITIAL INSPECTION: CRACKED FLOOR SUPPOR ON STA 1041 BTW X=15 AT PAX CABIN AREA (CPAX). SUMMARY OF NRC S/N 00836: CRACKED FLOOR SUPPORT ON STA 1041 BTW X=15 AT PAX CABIN AREA (CPAX) WAS REPLACED PER MD-90 SRM 51-30- 05 VOL.II. (LP#1463134)Jan 27, 2020 · N908DA · Doug MD9030 · Fuselage Main, Floor BeamSDR DALA2020012970679Frame · crackedCRACK ON RING PAN UPPER FWD EDGE AT STA Y= 674 RH SIDE. (CPAX) SUMMARY OF NRC 00281: RING PAN UPPER FWD EDGE AT STA Y= 674 RH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1462880)Jan 26, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020012970678Frame · crackedCRACK ON RING PAN UPPER FWD EDGE AT STA Y= 807 AND LOWER FWD EDGE STA Y=864 RH SIDE. (CPAX) SUMMARY OF NRC 00292: RING PAN UPPER FWD EDGE AT STA Y= 807 AND LOWER FWD EDGE STA Y=864 RH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1462863)Jan 26, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020012970677Frame · crackedCRACK ON RING PAN UPPER FWD EDGE AT STA Y= 731 RH SIDE. (CPAX) SUMMARY OF NRC 00282: RING PAN UPPER FWD EDGE AT STA Y= 731 RH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1462766)Jan 26, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020012960676Frame · crackedCRACK ON RING PAN UPPER AFT EDGE AT STA Y= 1288 LH SIDE. (CPAX) SUMMARY OF NRC 00138:RING PAN UPPER AFT EDGE AT STA Y= 1288 LH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1461939)Jan 26, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020012960675Frame · crackedINITIAL INSPECTION: CRACK ON RING PAN LOWER FWD EDGE AT STA Y= 1288 LH SIDE. (CPAX) SUMMARY OF NRC 00137:RING PAN LOWER FWD EDGE AT STA Y= 1288 LH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1461934)Jan 26, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020012960674Frame · crackedCRACK ON RING PAN LOWER AFT EDGE AT STA Y= 943, Y=674 AND Y= 845 LH SIDE. (CPAX) SUMMARY OF NRC 00136:RING PAN LOWER AFT EDGE AT STA Y=943, Y=674 AND Y= 845 LH SIDE. WERE REPAIRED PER MD-90 SRM-56-20-02 FIGURE 2 (1461887)Jan 26, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020012960673Frame · crackedCRACK ON WINDOW RING PAN, UPPER FORWARD EDGE AT STA Y=984 AND Y=674 LH SIDE. (CPAX) SUMMARY OF NRC 00184:WINDOW RING PAN, UPPER FORWARD EDGE AT STA Y=984 AND Y=674 LH SIDE WAS REPAIRED PER MD-90 SRM-56-20-02 FIGURE2 (1461878)Jan 26, 2020 · N908DA · Doug MD9030 · Flight Compartment WindowsSDR DALA2020012960672Frame · crackedCRACK ON RING PAN UPPER FWD EDGE AT STA Y= 984 RH SIDE. (CPAX) SUMMARY OF NRC 00293: RING PAN UPPER FWD EDGE AT STA Y= 984 RH SIDE WAS REPAIRED PER MD 90 VOL I SRM 56-20-02 TYPE C FIGURE 3Jan 26, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020020300830Seat Track · corrodedCORROSION ON LH SEAT TRACK X=54 STA 1095- 1100, 1110-1115, 1130-1135,1140-1145 AND 1155-1160 MRB 53-211-02 (CPAX) SEAT TRACK X=54 LH ON STA 1095 TO STA 1160 WAS REPLACED PER MD-90 SRM VOL. II 51-30-01 (1460540)Jan 25, 2020 · N908DA · Doug MD9030 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020012960671Frame · crackedCRACK ON RING PAN UPPER AFT EDGE AT STA Y= 1231 RH SIDE. (CPAX) SUMMARY OF NRC 00284: RING PAN UPPER AFT EDGE AT STA Y= 1231 RH WAS REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2Jan 25, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020012960670Frame · crackedCRACK ON RING PAN LOWER FWD EDGE AT STA Y= 712 AND LOWER AFT EDGE STA Y=1079 AND Y=1098 RH SIDE. (CPAX) RING PAN LOWER FWD EDGE AT STA Y= 712 AND LOWER AFT EDGE STA Y=1079 AND Y=1098 RH WERE REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2 (1461639)Jan 25, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020012960669Frame · crackedCRACK ON RING PAN UPPER AFT EDGE AT STA Y= 1250 RH SIDE. (CPAX) SUMMARY OF NRC 00294 RING PAN UPPER AFT EDGE AT STA Y= 1250 RH WAS REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2 (1461632)Jan 25, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020012960668Frame · crackedCRACK ON LOWER AFT RING PAN STA Y= 332 AND 636 AT PAX CABIN SUMMARY OF NRC 00135 LOWER AFT RING PAN STA Y= 332 AND 636 WERE REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2 LOG-PAGE UPDATED (1461624)Jan 25, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020020300829Cusp Web · corrodedCORROSION LEVEL 2 OUT OF LIMITS ON LH CUSP WEB STA 1079- 1098 AND 1117-1136 BTW X=54 AND X=60 ON REFERENCE AT NRC 269 MRB 53?211?01 (CPAX) : LH CUSP WEB STA 1079-1098 AND 1117-1136 WERE REPAIRED PER MD-90 SRM VOL. I 53-20-02 FIG 18. (1459776)Jan 24, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020012940667Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA 160-200 AND X =-44 AT FWD WET AREA MRB SUMMARY OF NRC S/N 00375 CORROSION LEVEL 2: FLOOR SUPPORT STA 160-200 AND X=-44 AT FWD WET AREA OUT LIMITS WAS REPLACED PER MD -90 SRM 51-30-02 VOL. II (1459079)Jan 24, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020012940680Starter · not reportedAT GATE W/APU AND PACKS ON STRONG ODOR INSIDE CABIN, TAIL CONE AND OUTSIDE NEAR APU COMPARTMENT. SMELL BEST DESCRIBED AS ACRID CHEMICAL BURNING. R/R APU STARTER PER MD90 AMM 49-44. WILL REQ LEAK CHECK. ALSO REQ RELAY R2-63, R2-792 (AMT 794502). R/R LT AND RT SJan 23, 2020 · N916DN · Doug MD9030 · APU Start/Ignition SystemSDR DALA2020012100405Cusp Web · corrodedINITIAL INSPECTION: CORROSION ON LH CUSP WEB STA 960-965, 984- 1003, 1003-1022, 1022-1041, 1041-1060 AND 1060-1079 BTW X=54 AND X=60 MRB 53?211?01 (CPAX) C/A SUMMARY OF NRC S/N 00268: CORROSION LEVEL 1 ON LH CUSP WEB STA 960-965, 984-1003, 1003-1022, 1022-1041Jan 21, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020012100407Cusp Web · crackedINITIAL INSPECTION: CRACKED LH CUSP WEB ON STA 875 BTW X=54 AND X=60 (CPAX) C/A LH CUSP WEB ON STA 875 BTW X=54 TO X=60 WAS REPAIRED PER MD 90 SRM 53-20-02 PAR. 6 FIG. 6 VOL. I. (1454253)Jan 20, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2019123007624Beam · crackedCRACKED BEAM NR 4 AT THE FWD GALLEY SERVICE DOOR. THE BEAM WAS REPLACED IAW SRM, VOL. II 51-30-01, 51-30-02, AND 51-30 -05.Dec 30, 2019 · N908DA · Doug MD9030 · Galley DoorsSDR DALA2019123007623Beam · not reportedBEAM NR 4 AT FWD GALLEY SERVICE DOOR (R1) WAS REPLACED IAW SRM, VOL. II 51-30-01, 51-30-02 AND 51-30 -05. THE BEAM NR 4 AT FWD GALLEY SERVICE DOOR (R1) WAS REPLACED IAW SRM, VOL. II 51-30-01, 51-30-02 AND 51-30 -05.Dec 30, 2019 · N908DA · Doug MD9030 · Galley DoorsSDR DALA2019121807401O-Ring · failedSHIP 9260 - TO IAH - DURING TAXI IN, JUST AS THE APU STARTED, GOT A STRONG FUEL ODOR IN THE CABIN TO THE COCKPIT NO FUMES SHUT DOWN THE APU ODOR DISSIPATED SLOWLY. FOUND FUEL LEAK BELOW APU AT GATE. / C/A FOUND APU FUEL CONTROL BOWL "O" RING EXPOSED & BOWL MOUDec 17, 2019 · N960DN · Doug MD9030 · APU Engine Fuel and ControlSDR DALA2019121607317Battery · inoperativeROW 25 EMERGENCY LIGHT OUT C/A R/R BATTERY ASSY PER MD90 AMM 33-51. OPS CHECK IS GOOD AT THIS TIME. (6615064)Dec 16, 2019 · N919DN · Doug MD9030 · Emergency LightingSDR DALA2019121607316Blade · missingCAPTS WIPER BLADE MISSING ON ARRIVAL LOG-PAGE UPDATED @ 14DEC19 0835 UTC 02 CORR BY SIEKIERA 00705577 PVD 14DEC19 ATA 3043 RII: N ENTR 00705577 W REPLACED CAPT WINDSHIELD WIPER AND ARM PER MD90 AMM 30-43 INSPECTED AROUND WINDSHIELD AREA NO VISUAL DAMAGE NOTED Dec 14, 2019 · N934DN · Doug MD9030 · Windshield/Door Rain/Ice RemovalSDR DALA2020010300036Door · missingAFT CONDITIONED AIR DUCT DOOR MISSING C/A INSTALLED GROUND AIR CONNECTION DOOR PER MD90 AMM 21-28. CDL/ PLACARD REMOVED (6405062)Dec 11, 2019 · N924DN · Doug MD9030 · Air Conditioning DoorsSDR DALA2020010980117Tab · damagedPD: TAB DAMAGED, CORNER DAMAGED, BEARING DAMAGE CA: REPAIRED PER MD 90 SRM 55-21-01 VOL 1 PARA 11,CMM 27-30-25 REPAIR8-1 / WEIGHT:4.52 LBSDec 7, 2019 · Doug MD9030 · Elevator, Tab StructureSDR DALA2019120607128Unknown · fumesDURING TAXI IN AFTER LANDING CLE, AFT FLT ATTENDANT REPORTED A HAZE/ SMOKE IN CABIN FROM ABOUT MIDWAY TO THE AFT OF CABIN. ONE FLIGHT ATTENDANT SAID IT HAD AN ACID/ACRID SMELL. THE HAZE DISAPATED BY THE TIME WE ARRIVED AT GATE. THERE WERE NO PASSENGER COMPLAINDec 6, 2019 · N915DN · Doug MD9030 · Air Distribution System
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