Douglas DC-9-41

Service difficulty reports · 2,671

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duckdb -csv -c "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 = 'DC941'
  ORDER BY difficulty_date DESC"

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SDR ABXA9700687Bearing Cup · corrodedDURING C-CHECK, THE RUDDER BEARING SUPPORT CUP WAS FOUND CORRODED. THE CUP WAS REPLACED IAW DC-9 SRM 51-30-2.Dec 28, 1996 · N969AX · Doug DC941 · Rudder StructureSDR ABXA9700686Bulkhead Door · crackedDURING C-CHECK, WHILE ACCOMPLISHING S/B 53-137 A CRACK WAS FOUND IN THE UPPER RT DOOR CORNER OF THE AFT PRESSURE BULKHEAD. THE BULKHEAD WAS REPAIRED IAW REA D953-17604-MR.Dec 28, 1996 · N969AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9700379Tr Bucket · crackedDURING C-CHECK, THE LOWER THRUST REVERSER BUCKET WAS FOUND CRACKED. THE BUCKET WAS REPLACED IAW DC9 MM 78-30-2.Dec 19, 1996 · N975AX · Doug DC941 · Engine Thrust ReverserSDR ABXA9700376Skin · damagedDURING C-CHECK, THE FUSELAGE SKIN ON THE AFT SIDE OF THE FWD ENTRY DOOR LOWER CORNER WAS FOUND DAMAGED. THE SKIN WAS REPAIRED IAW REA D953-17518.Dec 19, 1996 · N975AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9700363Fitting · corrodedDURING C-CHECK, THE AFT JACK PAD ATTACH FITTING WAS FOUND CORRODED. THE FITTING WAS REPLACED IAW DC-9 SRM 51-30-2.Dec 19, 1996 · N975AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9700359Frame · crackedDURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE MAIN FRAME AT STA 737 LEFT WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW S/B 53-131 AND REA D953-17522-MR.Dec 19, 1996 · N975AX · Doug DC941 · Fuselage Main, FrameSDR ABXA9700357Seat Track · corrodedDURING C-CHECK, THE SEAT TRACK AT STA 195RBL 44, WAS FOUND CORRODED. THE SEAT TRACK WAS REPAIRED IAW REA D953-17543-DE AND THE DC9 SRM. 51-30-1.Dec 19, 1996 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA9600685Light Plate · defectiveSMOKE APPEARED AT COMPARATOR RESET BUTTON, LEFT AC ISOLATED AND OPERATIONS WERE NORMAL. REPLACED COMPARATOR TEST LIGHT PANEL IAW DC-9 M.M. 33-10.Dec 19, 1996 · N990AX · Doug DC941 · Flight Compartment LightingSDR ABXA9700878Spoiler · delaminatedTHE LEFT INBOARD SPOILER HAD SEVERAL AREAS OF DELAMINATION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.Dec 18, 1996 · N960AX · Doug DC941 · SpoilersSDR ABXA9700422Carriage · wornDURING C-CHECK, THE FLAP CARRIAGE ROLLERS WERE FOUND WORN. THE CARRIAGE WAS REPLACED IAW DC9 SUP MM 27-51-5.Dec 18, 1996 · N975AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9700381Frame · crackedDURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE FUSELAGE MAIN FRAME AT STA 737LT WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW REA D953-17522-MR AND S/B 53-131.Dec 18, 1996 · N975AX · Doug DC941 · Fuselage Main, FrameSDR ABXA9700380Angle · crackedDURING C-CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC9 SRM 54-04, FIG.10.Dec 18, 1996 · N975AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9700377Angle · crackedDURING C CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC-9 SSRM DRAWING NR K-05683.Dec 18, 1996 · N975AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9700368Doubler · crackedDURING C-CHECK, THE FUSELAGE SKIN DOUBLER AT THE MAIN ENTRY DOOR WAS FOUND CRACKED. THE DOUBLER WAS REPLACED IAW DC-9 SRM 51-30-5.Dec 18, 1996 · N975AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9700365Damper Crank · corrodedDURING C-CHECK, THE AILERON DAMPER CRANK WAS FOUND CORRODED. THE DAMPER WAS REPLACED IAW DC-9 MM 27-10-4.Dec 18, 1996 · N975AX · Doug DC941 · Aileron Control SystemSDR ABXA9700364Vane · delaminatedDURING C-CHECK, THE FLAP AFT MOVEABLE VANE WAS FOUND DELAMINATED. THE VANE WAS REPLACED IAW DC-9 MM 27-51-2.Dec 18, 1996 · N975AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9700361Vane · corrodedDURING C-CHECK, THE FLAP FORWARD MOVEABLE VANE WAS FOUND CORRODED. THE VANE WAS REPLACED IAW DC-9 MM 27-51-1.Dec 18, 1996 · N975AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9700360Doubler · crackedDURING C-CHECK, THE ENGINE PYLON BULKHEAD DOUBLER WAS FOUND CRACKED. THE DOUBLER WAS REPLACED IAW DC-9 SRM 51-30-5.Dec 18, 1996 · N975AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9700356Frame · crackedDURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE MAIN FRAME AT STA 737 RT, WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW REA DC953-17522-MR.Dec 18, 1996 · N975AX · Doug DC941 · Fuselage Main, FrameSDR ABXA9700355Frame · crackedDURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE MAIN FRAME AT STA 737 LT WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW REA DC953-17522-MR.Dec 18, 1996 · N975AX · Doug DC941 · Fuselage Main, FrameSDR ABXA9700354Angle · crackedDURING C CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC9 SRM 54-04, FIG.10.Dec 18, 1996 · N975AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9700676Vane · corrodedTHE RIGHT WING FORWARD FLAP VANE WAS CORRODED ALONG THE TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.Dec 17, 1996 · N975AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9700674Vane · delaminatedTHE RIGHT AFT FLAP VANE HAD LARGE AREA'S OF DELAMINATION ON BOTH THE UPPER AND LOWER TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC9 SRM.Dec 17, 1996 · N975AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9700378Cowl Frame · gougedDURING C-CHECK, THE UPPER COWL INBOARD LONGERON FRAME WAS FOUND GOUGED. THE COWL WAS REPAIRED IAW ABX DWG K05013.Dec 17, 1996 · N975AX · Doug DC941 · Engine Cowling SystemSDR ABXA9700375Angle · crackedDURING C-CHECK, THE PYLON UPPER FUSELAGE ATTACH ANGLE AT STA 1072, WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC-9 SRM 54-04, FIG.10.Dec 17, 1996 · N975AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9700374Tr Fairing · crackedDURING C-CHECK, THE LOWER THRUST REVERSER BUCKET FAIRING WAS FOUND CRACKED. THE FAIRING WAS REPLACED IAW DC-9 SRM 51-30-2.Dec 17, 1996 · N975AX · Doug DC941 · Engine Thrust ReverserSDR ABXA9700373Angle · crackedDURING C-CHECK, THE PYLON UPPER SPAR CAP ANGLE AT THE OUTBOARD END WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW REA D954-17521.Dec 17, 1996 · N975AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9700370Angle · crackedDURING C CHECK, THE SEAT TRACK ATTACH ANGLE AT STA 1041 LONG 27 LT, WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC-9 SRM 51-30-1 AND 51-30-5.Dec 17, 1996 · N975AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9700358Angle · crackedDURING C-CHECK, THE VENTRAL STAIR RIGHT HINGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC9 SRM 51-10-4.Dec 17, 1996 · N975AX · Doug DC941 · Fuselage Miscellaneous StructureSDR TWAA9615601Battery Pack · dischargedSTL - DURING CRUISE AISLE EGRESS LIGHTS ILLUMINATED AT SEAT ROWS 14 THROUGH 18. FOUND BATTERY PACK, MFG P/N 5822-2, WEAK. REPLACED BATTERY PACK. EGRESS LIGHTING SYSTEM OPERATION THEN CHECKED NORMAL. (M)Dec 16, 1996 · N933L · Doug DC941 · Emergency LightingSDR ABXA9700874Vane · delaminatedTHE LEFT INBOARD FIXED FLAP VANE WAS DELAMINATED IN THE UPPER MID-AREA. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.Dec 16, 1996 · N960AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9700372Tr Fairing · crackedDURING C-CHECK, THE UPPER THRUST REVERSER BUCKET FAIRING WAS FOUND CRACKED. THE FAIRING WAS REPLACED IAW DC-9 SRM 51-30-2.Dec 16, 1996 · N975AX · Doug DC941 · Engine Thrust ReverserSDR ABXA9700371Carriage · wornDURING C-CHECK, THE FLAP CARRIAGE ASSEMBLY WAS FOUND WORN. THE CARRIAGE ASSEMBLY WAS REPLACED IAW DC-9 SUP MM 27-51-5.Dec 16, 1996 · N975AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9700369Guide Rail · gougedDURING C-CHECK, THE GUIDE RAIL AT STA 218 LBL 45, WAS FOUND GOUGED. THE GUIDE RAIL WAS REPLACED IAW DC-9 SRM.Dec 16, 1996 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA9700366Tab · wornDURING C-CHECK, THE AILERON TRIM TAB INBOARD HINGE WAS FOUND WORN. THE TRIM TAB WAS REPLACED IAW DC-9 MM 27-10-5.Dec 16, 1996 · N975AX · Doug DC941 · Aileron TabsSDR 9626859763Battery Pack · dischargedDURING LINE CHECK, FOUND MID SECTION EMERGENCY LIGHTS BY EMERGENCY EXIT DOORS INOPERATIVE. REPLACED 05-903 BATTERY PACK AND CHARGER. OPERATION CHECKS GOOD.Dec 16, 1996 · N763NW · Doug DC941 · Emergency LightingSDR ABXA9700362Seat Track · corrodedDURING C CHECK, THE SEAT TRACK AT STA 190 RBL 22 WAS FOUND CORRODED. THE TRACK WAS REPAIRED IAW DC-9 SRM 53-05, FIG. 4A.Dec 15, 1996 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA9700367Depressor · crackedDURING C-CHECK, THE MAIN LANDING GEAR OUTBOARD DOOR SEAL DEPRESSOR WAS FOUND CRACKED. THE DEPRESSOR WAS REPLACED IAW DC-9 SRM 51-30-2.Dec 14, 1996 · N975AX · Doug DC941 · Landing Gear DoorsSDR 9626429762Strut · reqd serviceAFTER TAKEOF, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR EXTENDED NORMALLY BUT GEAR HANDLE WOULD NOT GO UP AGAIN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. AIRCRAFT JACKED AND NOSE STRUT WAS RESERVICED, OPERATIONAL CHEDec 14, 1996 · N762NW · Doug DC941 · Nose/Tail Landing Gear Strut/AxleSDR ABXA9701065Door · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING CENTER BUTE DOOR HEAVILY CORRODED ON INNER AND OUTER SURFACES. REMOVED AND REPLACED BUTE DOOR ASSY IAW DC9 MAINTENANCE MANUAL CHAPTER 57-20-3.Dec 13, 1996 · N960AX · Doug DC941 · Wing, Plate/SkinSDR ABXA9700803Intercostal · crackedDURING C-CHECK, THE LT INTERCOSTAL AT CANTED FRAME STA 1244 WAS FOUND CRACKED. THE INTERCOSTAL WAS REPLACED IAW DC9 SRM.Dec 11, 1996 · N966AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9700802Spoiler · delaminatedDURING C-CHECK, THE INBOARD SPOILER PANEL AT THE CENTER HINGE WAS FOUND DELAMINATED. THE SPOILER WAS REPLACED IAW DC9 MM.Dec 11, 1996 · N966AX · Doug DC941 · SpoilersSDR ABXA9700677Vane · delaminatedTHE RIGHT WING INBOARD FLAP VANE HAD DELAMINATION BETWEEN THE CENTER RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.Dec 11, 1996 · N966AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9700194Panel · delaminatedDURING C-CHECK, HORIZONTAL STABILIZER PANEL NR 3806 WAS FOUND DELAMINATED, NR CF-808. REPLACED THE PANEL IAW DC-9 SRM 51-10-4.Dec 11, 1996 · N966AX · Doug DC941 · Horizontal Stabilizer, Plate/SkinSDR ABXA9700193Panel · chafedDURING C-CHECK, VERTICAL STABILIZER SKIN PANEL WAS FOUND CHAFED NEXT TO HORIZONTAL STABILIZER, NR CF-818. REPLACED THE SKIN PANEL IAW DC-9 SRM 51-10-4.Dec 11, 1996 · N966AX · Doug DC941 · Vertical Stabilizer, Plate/SkinSDR ABXA9700192Linkage · wornDURING C-CHECK, THE LEFT LANDING GEAR OUTBOARD DOOR HINGE AND LINKAGE ASSEMBLY WERE FOUND WORN. REPLACED THE LINKAGE ASSEMBLY IAW DC-9 MM 32-12-1.Dec 11, 1996 · N966AX · Doug DC941 · Landing Gear Door Retract SectionSDR ABXA9700191Linkage · wornDURING C-CHECK, THE RIGHT LANDING GEAR OUTBOARD DOOR LINKAGE ASSEMBLY WAS FOUND WORN, NR CF-769. REPLACED THE LINKAGE ASSEMBLY IAW OHM 32-10-6.Dec 11, 1996 · N966AX · Doug DC941 · Landing Gear Door Retract SectionSDR ABXA9700190Door · delaminatedDURING C-CHECK , THE RIGHT WING BUTE DOOR NR 1603 WAS FOUND DELAMINATED, NR UD-004. REPLACED THE RIGHT WING BUTE DOOR NR 1603 IAW DC-9 M.M 57-20-3.Dec 11, 1996 · N966AX · Doug DC941 · Wing Miscellaneous StructureSDR TWAA9615202Lights · inoperativeSTL - FLT 550 - DURING PRE-FLIGHT, CABIN EGRESS LIGHTS WERE INOPERATIVE. RESET ARM AND CHANGE CIRCUIT BREAKER. OPERATION CHECK NORMAL. OP-15 - 11-15-96 - STL. (X)Dec 8, 1996 · N933L · Doug DC941 · Emergency LightingSDR ABXA9700199Panel · delaminatedDURING C-CHECK, THE RIGHT WING INBOARD UPPER AFT BONDED PANEL WAS FOUND DELAMINATED, NR CF-908. REPLACED THE RIGHT WING INBOARD UPPER AFT BONDED PANEL IAW DC-9 SRM 51-10-4.Dec 8, 1996 · N966AX · Doug DC941 · Wing, Plate/Skin
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