Douglas DC-9-33F

Service difficulty reports · 1,681

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = 'DC933F'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ABXA9500435Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 30 CRACKED AT STA 415. REPLACED LONGERON IAW DC-9 SRM 51-30-5, 51-30-7 AND 51-30-1.Apr 22, 1995 · N933AX · Doug DC933F · Fuselage Main, Longeron/StringerSDR ABXA9500369Link · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR LINK BEARING TO HAVE EXCESSIVE PLAY. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 32-106.Apr 22, 1995 · N930AX · Doug DC933F · Landing Gear Door Retract SectionSDR ABXA9500367Bushing · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR DOUBLE TO SINGLE LINK TO HAVE EXCESSIVE PLAY. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.Apr 22, 1995 · N930AX · Doug DC933F · Landing Gear DoorsSDR ABXA9500366Fitting · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR ARTICULATING DOOR LINK ARM TO HAVE EXCESSIVE PLAY. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6.Apr 22, 1995 · N930AX · Doug DC933F · Landing Gear DoorsSDR ABXA9500427Floorbeam · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON THE LOWER FLOORBEAM ATTACH TEE AT STA 756, FROM APPROXIMATELY X EQUALS -18 TO OUTBOARD END. REPAIRED IAW ABX REA D953-11425-MR.Apr 21, 1995 · N933AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA9500437Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 30 CRACKED AT STA 579. REPLACED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5.Apr 20, 1995 · N933AX · Doug DC933F · Fuselage Main, Longeron/StringerSDR ABXA9500428Panel · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON THE UPPER SIDE OF THE PRESSURE PANEL AT X EQUALS A D953-11427-MR.Apr 17, 1995 · N933AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA9500334Eel Battery · dischargedEMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERIES. OPS CHECKED NORMAL IAW DC-9 SUPP MM 33-53-00.Apr 17, 1995 · N930AX · Doug DC933F · Emergency LightingSDR ABXA9500442Link · crackedDURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE RIGHT WING INBOARD SPOILER DRIVE LINK CRACKED. REPLACED LINK IAW DC-9 MM 27-61-1.Apr 15, 1995 · N933AX · Doug DC933F · Drag Control SystemSDR ABXA9500426Beam · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON A FLOORBEAM AT STA 737R RBL 44. REPAIRED BEAM IAW ABX REA D953-11422-MR.Apr 14, 1995 · N933AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA9500443Link · crackedDURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE RIGHT WING OUTBOARD SPOILER DRIVE LINK CRACKED. REPLACED THE LINK IAW DC-9 MM 27-61-1.Apr 13, 1995 · N933AX · Doug DC933F · Drag Control SystemSDR ABXA9500441Fitting · crackedDURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE RIGHT WING INBOARD SPOILER AFT ATTACH FITTING CRACKED. REPLACED THE FITTING IAW DC-9 MM 27-61-1.Apr 13, 1995 · N933AX · Doug DC933F · Drag Control SystemSDR ABXA9500440Link · crackedDURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE LEFT WING INBOARD SPOILER DRIVE LINK CRACKED. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 27-61-1.Apr 13, 1995 · N933AX · Doug DC933F · Drag Control SystemSDR ABXA9500439Link · crackedDURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE LEFT WING OUTBOARD SPOILER DRIVE LINK CRACKED. REPLACED IAW DC-9 SUPP MM 27-61-1.Apr 11, 1995 · N933AX · Doug DC933F · Drag Control SystemSDR EIAA9513Skin · birdstrikeON APPROACH TO DEN, BIRD STRIKE OCCURRED ON LEFT WING. THE BIRD IMPACTED THE NR 2 SLAT AND THE FIXED LEADING EDGE AT WING STATION XFS EQUALS 250. SLAT WAS DAMAGED AND THE WING LEADING EDGE WAS DENTED JUST FORWARD OF THE ROUND ACCESS PANEL. (M)Apr 6, 1995 · N944F · Doug DC933F · Wing, Plate/SkinSDR ABXA9500214Doubler · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03; S.B. 56-11, REV. 3, FOUND SMALL CRACKS AROUND FASTENERS ON DOUBLER. REPLACED DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-1.Mar 9, 1995 · N934AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500209Skin · dentedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AT LONGERON 19R AT STA 207. REPAIRED IAW ABX REA D953-11089-MR.Mar 7, 1995 · N934AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA9500215Frame · damagedDURING C-CHECK INSPECTION, FOUND DRILL HOLE IN FUSELAGE FRAME STA 756 BETWEEN LONGERONS 7L AND 8L. REPAIRED IAW ABX REA D953-11085-MR.Mar 6, 1995 · N934AX · Doug DC933F · Fuselage Main, FrameSDR ABXA9500212Intercostal · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND CORROSION ON UPPER DOOR JAMB AT AFT CORNER. REMOVED CORROSION, TREATED AND PRIMED AREA IAW DC-9 SRM 51-10-3.Mar 1, 1995 · N934AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500213Blkhd Jamb · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 85-01-02, S.B. 53-137 FOUND THE AFT PRESSURE BULKHEAD UPPER DOOR JAMB LEFT AND RIGHT CORNERS HAVE BEND RADIUS CRACKS IN THE FORWARD FLANGE WHICH EXTEND BEYOND THE STOP DRILLS. REPAIRS ARE ACCEPTABLE AS IS PEFeb 28, 1995 · N934AX · Doug DC933F · Fuselage Main, BulkheadSDR ABXA9500211Frame · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 78-07-05, S.B. 53-131 FOUND FRAME STA 699 RIGHT, CRACKED ON THE FORWARD LOWER FLANGE. CRACK IS WITHIN LIMITS OF DC-9 S.B. 53-131.Feb 28, 1995 · N934AX · Doug DC933F · Fuselage Main, FrameSDR ABXA9600355Tr Drive Link · crackedDURING COMPLIANCE OF AD 75-14-06, AD 90-18-03; SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND THE NR 2 THRUST REVERSER OUTBOARD UPPER DRIVER LINK HAD A CRACK INDICATION. REPLACED THE NR 2 THRUST REVERSER OUTBOARD UPPER DRIVER LINK IAW DC-9 MM 78-31-5. LINK CRACKEFeb 20, 1995 · N931AX · Doug DC933F · Engine Thrust ReverserSDR EIAA9507Connector · looseDEN - ON LANDING GEAR EXTENSION LEFT MAIN LANDING RED LIGHT AND GEAR DOWN GREEN LIGHT WOULD NOT ILLUMINATE. AFTER NORMAL LANDING, THE RED LIGHT AND GEAR DOWN GREEN LIGHT STILL WOULD NOT ILLUMINATE. REPLACED PIN'S AT CONNECTOR P1-132 AT LEFT MAIN DOWNLOCK SWIFeb 8, 1995 · N933F · Doug DC933F · Landing Gear Position and WarningSDR ABXA9500078Wire · openWHEN LANDING GEAR EXTENDED, RIGHT GEAR UNSAFE AND RIGHT LANDING GEAR LIGHTS DID NOT ILLUMINATE. RECYCLED GEAR. RIGHT LANDING GEAR UNSAFE LIGHT DID NOT ILLUMINATE. RIGHT LANDING GEAR LIGHT ILLUMINATED. REPAIRED WIRE NR 2G206E24 NEAR TERMINAL BOARD S3-66 PERFeb 8, 1995 · N933AX · Doug DC933F · Landing Gear Position and WarningSDR EIAA9506Handle · lack of lubeLEFT MAIN GEAR DOWN, GREEN LIGHT INOPERABLE. DID NOT WORK ON GEAR EXTENSION. WILL NOT TEST ON GROUND. COULD NOT PULL EMERGENCY GEAR EXTENSION LEVER TO FULL TRAVEL UPWARD. BEGAN TO BIND WHEN PULLED UP ON HALF OF FULL TRAVEL. RETURNED TO SECURED POSITION BEFeb 7, 1995 · N933F · Doug DC933F · Landing Gear Position and WarningSDR ABXA9500210Spar Cap · corrodedDURING C-CHECK INSPECTION, FOUND RIGHT WING REAR SPAR LOWER T-CAP HAD LEVEL II CORROSION AT WING TIP. REPAIRED IAW ABX REA D957-11076-MR.Feb 4, 1995 · N934AX · Doug DC933F · Wing SparSDR EIAA9602Pressurization · malfunctionedOAK - DESCENT INTO SLC TURNED ON AIRFOIL A/I AT APPROXIMATELY FL 23.0, CABIN RATE OF CLIMB WENT APPROX FULL UP WITH OUTFLOW VALVE FULL CLOSED. TURNED OFF WING A/I AND CABIN PRESSURE RETURNED TO NORMAL. (M)Jan 31, 1995 · N944F · Doug DC933F · Cabin Pressure Control SystemSDR ABXA9500064Dn Lock Sw · corrosionLEFT MAIN LANDING GEAR DOWN INDICATOR DID NOT ILLUMINATE ON INITIAL GEAR EXTENSION. CYCLED LANDING GEAR AND LIGHT ILLUMINATED. FOUND CORROSION IN THE LEFT GEAR DOWNLOCK SWITCH AND MOISTURE IN THE CANNON PLUG. CLEANED CORROSION FROM SWITCH AND REMOVED MOISTUJan 30, 1995 · N930AX · Doug DC933F · Landing Gear Position and WarningSDR EIAA9503Spar Cap · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON RIGHT UPPER REAR SPAR CAP AFT FLANGE XRS -133 TO -137. CORROSION BLENDOUT EXCEEDED DC9 SRM LIMITS. THE BLENDED AREA WAS TEMPORARILY REPAIRED USING 7075-T6 DOUBLERS, ANGLES AND FILLERS INSTALLED WET WITH SEALANT. Jan 14, 1995 · N933F · Doug DC933F · Wing SparSDR ABXA9500003Eel Battery · dischargedCOCKPIT EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERIES. OPS CHECKED GOOD IAW DC-9 M.M. 33-53-0.Jan 9, 1995 · N935AX · Doug DC933F · Emergency LightingSDR ABXA9500073Frame · gougedDURING COMPLIANCE OF A.D. 79-24-01; S.B. 53-127, FOUND GOUGE AT 10 O'CLOCK POSITION ON PLUG DOOR STOP. BLENDED OUT GOUGE AT 10 O'CLOCK POSITION IAW DC-9 SRM 51-01.Jan 7, 1995 · N935AX · Doug DC933F · Fuselage Main, Bulkhead
Back to Douglas DC-9-33F