N516DA, cancelled Mar 18, 2003

Service difficulty reports · 78

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N516DA' AND deregistration_id = 'N516DA-2003-03-18'
  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 DL72S021376Shim · out of positionREPAIR FOR MIGRATED SHIM, INSPECTION OF LT WING INBD FLAP INBD FLAP TRACK REVEALED A MIGRATED LAMINATED SHIM. THE CONDITION IS TYPICAL OF THAT DOCUMENTED PER BAC S/B 727-57-0178 AND AD 90-07-05. THE SHIM WAS MIGRATED BEYOND THE ALLOWABLE LIMITS OF THE S/B ANNov 23, 2002 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S021264Transceiver · malfunctionedATB, WX RADAR C/B POPPED TWICE. REPLACED WX RADAR R/T TEST PATTERN NORMAL - OPERATED IN WX MOD OBTAINED TARGETS, ALL OPS NORMAL.Oct 30, 2002 · N516DA · Boeing 727232 · Weather Radar SystemSDR DL72S021208Skin · crackedFUSELAGE / SKIN / FS 681-740 / STRG. 4R / SKIN LAP SPLICE : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 & 740 REVEALED CRACK INDICATIONS. INTERNAL MFEC INSPECTION REVEALED Oct 16, 2002 · N516DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S021207Skin · crackedFUSELAGE / SKIN / FS 481-681 / STRG. 4R / SKIN LAP JOINT : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP JOINT REVEALED CRACK INDICATIONS BETWEEN FS 481 & 681. INTERNAL MFEC INSPECTION REVEALED Oct 16, 2002 · N516DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S021198Skin · crackedFUSELAGE / SKIN / FS 1070-1090 / STRG. 4R / SKIN LAP JOINT: CRACK REPAIR LFEC INSPECTIONS OF THE STRINGER 4R SKIN LAP JOINT REVEALED A CRACK INDICATION. INTERNAL MFEC INSPECTION DETERMINED A SINGLE Oct 15, 2002 · N516DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S020422Mount · crackedINSPECTION OF THE FWD ENGINE MOUNT SUPPORT FITTING ON THE NR 3 ENGINE PYLON PER AD 97-05-08 REVEALED A CRACK IN HOLE LOCATION -D-. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND AN ADDITIONAL INSURANCE CUT TAKEN. THE REWORK WAS ACCOMPLISHED PER FED EX S/B 20Apr 9, 2002 · N516DA · Boeing 727232 · Engine Mount SectionSDR DL72S020401Casting · crackedNR 7 SPOILER LWR CASTING REPAIR CRACKED AT LWR WING ATTACH. REPAIRED PER MM 57-20-022-8.Apr 3, 2002 · N516DA · Boeing 727232 · SpoilersSDR DL72S020398Stiffener · crackedNR 7 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. REPLACING STIFFENER PER M/M 57-20-021-8.Apr 3, 2002 · N516DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S011902Switch · intermittentL/E FLAP LIGHT ILLUMINATED WHEN WING ANTI ICE SELECTED ON. REPLACED NR 4 AND NR 5 L/E FLAP POSITION XMITTERS.Dec 6, 2001 · N516DA · Boeing 727232 · Leading Edge Slat Position Indicating SystemSDR DL72S011793Actuator · leakingLOST A SYSTEM HYDRAULICS ON CLIMBOUT FROM ABQ. LOST PRESSUREAND QUANTITY BOTH TO ZERO. _REPLD NBR 3 L/E FLAP ACTUATORNov 12, 2001 · N516DA · Boeing 727232 · Hydraulic Power SystemSDR DL72S011518Bulkhead · crackedFUSELAGE / BULKHEAD / FS 351.2 / LBL 5 : WEB CRACK REPAIR THE FS 351.2 BULKHEAD WEB WAS FOUND CRACKED AT LBL 5 AT A DAMAGED NLG UPLOCK FITTING ATTACH POINT. THE WEB AND LOCAL BULKHEAD CHORD WERE Sep 6, 2001 · N516DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S011501Support · crackedON FINAL WHEN LDG GEAR EXTENDED -A-SYS HYD FAILURE-COMPLETE-GEAR DOWN AND LOCKED FLAPS 30DGS-RAISED FLAP ELEC. TO 15DGS AND LANDED A/C- FOUND NOSEGEAR UPLCKACT.BRACKET CRACKED AND ACT.LINES DAMAGED-RPLCD BRACKET ACTUATOR LINES AND C/W ERA REPAIR TO STA351.5 WEAug 27, 2001 · N516DA · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72S011422Actuator · leakingON LANDING COMPLETE A SYSTEM HYD FAILURE. FOUND OVER CENTER ACTUATOR BULKHEAD FITTING BROKEN AND ACTUATOR LEAKING. CA REPLACED SAME.Aug 27, 2001 · N516DA · Boeing 727232 · Landing Gear ActuatorSDR DL72S011307Actuator · leakingON FINAL APPROACH PRIOR TO GEAR EXT WITH FLAPS 5 DEG AND HAD INDICATION OF A LOSS OF A SYSTEM HYD. REPLACED A SYSTEM FILTERS. REPLACED LEADING EDGE FLAP ACTUATOR FOR LEAKINGAug 9, 2001 · N516DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S011225Battery Pack · dischargedLEFT AFT OVERWING LIGHT INOP. REPLACED BATTERY PACK, CHECKS NORMAL.Jul 24, 2001 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S010419Light · will not testEMERG LIGHT AT REAR EXIT WOULD NOT TEST - REPLACED LIGHT RACKMar 13, 2001 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S010212Battery · dischargedEMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOP. REPLACED EMERGENCY EXIT LIGHT BATTERIES, OPS CKS OK.Feb 7, 2001 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S010138Skin · gougedTHE FUSELAGE SKIN JUST FWD OF THE FWD EDGE OF THE L1 DOOR CUTOUT WAS FOUND GOUGED MIDWAY BETWEEN THE UPPER AND LOWER HINGE CUTOUTS. BOTH HINGE CUTOUTS WERE PREVIOUSLY REPAIRED PER B727 S/B 53-0198. THE NEW DAMAGE WAS REMOVED WITH A 1 INCH CUTOUT. THE HINGEJan 24, 2001 · N516DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S010137Frame · crackedINSPECTIONS OF THE INNER CHORD, OUTER CHORD AND THE WEB OF THE C1 DOOR OPENING AFT FRAME REVEALED A 1.25 INCH CRACK IN THE OUTER CHORD BELOW THE NR 6 DOOR STOP, AN EXISTING STEEL SPLICE REPAIR FOR THE INNER CHORD, AND AN EXISTING ALUMINUM WEB REPAIR. THE EJan 24, 2001 · N516DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S010010Angle · crackedFOUND ON MV2 CHECK, .75 INCH CRACK NR 8 SLAT COVE SKIN ANGLE BELOW THE ANTI-ICE DUCT. REPAIRED PER MM 57-54-000-8.Jan 2, 2001 · N516DA · Boeing 727232 · Leading Edge DevicesSDR DL72S001559Duct · rupturedENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN CLIMB PASSING FL 250. COMPLETED WITH POM PROCEDURES, LIGHT REMAINED EXTINGUISH WITH THROTTLE AT IDLE. NR 1 BLEED SWITCH HAS NO EFFECT. DIVERTED TO DFW. FOUND HI STAGE PNEUMATIC -Y- DUCT IN PYLON RUPTURED. RAug 14, 2000 · N516DA · Boeing 727232 · Pneumatic Distribution SystemSDR DL72S000971Battery · inoperativeFOUND RT AFT CARGO DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED M957 BATTERY PACK. EMERGENCY LIGHTS OPS GOOD.May 16, 2000 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S000838Angle · crackedDURING SHOP VISIT, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 55 INCHES FROM THE I/B END. THE ANGLE WAS REPAIRED BY REPLACING A SECTION AND SPLICING PER MM 57-52-0, FIG 802.Apr 8, 2000 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S000837Angle · crackedDURING SHOP VISIT, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 37 INCHES FROM THE I/B END. THE ANGLE WAS REPAIRED BY REPLACING A SECTION OF THE ANGLE AND SPLICING IT WITH A DOUBLER PER MM 57-52-0, FIG 802.Apr 8, 2000 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992593Battery Pack · dischargedAFT CABIN EMERGENCY EXIT SIGN OVERHEAD INOP DURING LIGHTS TEST. REPLACED BATTERY PACK, OPS GOOD.Nov 21, 1999 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S992545Skin · cracked3/4 CRACK IN FUSELAGE SKIN STR 22R STA 1233. REPAIRED PER SRM 53-30-3 FIG 25.Nov 17, 1999 · N516DA · Boeing 727232 · Fuselage Structure (General)SDR DL72S992543Fslg Skin · crkdFUSELAGE SKIN CRACKED FS1090 BELOW STRINGER 17L. REPAIRED PER SRM 53-30-3 FIG 26.Nov 17, 1999 · N516DA · Boeing 727232 · Fuselage Structure (General)SDR DL72S992542Rib · crackedFOUND ON D1 LETTER CK, 1 INCH CRACK NR 2 SLAT NOSE RIB I/B SIDE OF ACTUATOR. REPAIRED PER MM 57-54-0.Nov 17, 1999 · N516DA · Boeing 727232 · Wing StructureSDR DL72S992512Battery Pack · dischargedON L/O, FOUND LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT STROBING. REPLACED BATTERY PACK, CKS OK.Nov 14, 1999 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S992197Transmitter · failedOUTBOARD FLAPS SPLIT WHEN FLAPS RETRACTED FROM 5 DEGS. REPLACED RIGHT OUTBOARD FLAP TRANSMITTER.Oct 4, 1999 · N516DA · Boeing 727232 · Trailing Flap Position Indicating SystemSDR DL72S992077Indicator · malfunctionedWHEN FLAPS WERE POSITIONED TO FLAPS 2, THE LEFT AND RIGHT OUTBOARD SHOWED SLIGHT ASYMMETRY (ABOUT 1 NEEDLE WIDTH) RAN CHECKLIST AND LOWERED FLAPS WITH ALTERNATE FLAP SWITCHES. FLAPS LOWERED TO 30 ON BOTH OUTBOARD, BUT INBOARD NOW SHOWED A SLIGHT SPLIT(ABOUT 5Sep 16, 1999 · N516DA · Boeing 727232 · Trailing Flap Position Indicating SystemSDR DL72S991920Tire · failedNR 1 TIRE BLOWN. REPLACED NR 1 WHEEL AND BRAKE. ALSO REPLACED NR 2 WHEEL.Aug 28, 1999 · N516DA · Boeing 727232 · TireSDR DL72S991039Switch · dirtyTAKEOFF WARNING HORN SOUNDED DURING POWER UP AND TAKEOFF WAS ABORTED AT 10 KTS. WARNING HORN ITEMS CYCLED AND SOUNDED AGAIN ON SECOND ATTEMPT. FOUND UPPER STAB TRIM SWITCH STICKING. CLEANED AND LUBED SWITCH. TAKEOFF WARNING TEST NORMAL.May 11, 1999 · N516DA · Boeing 727232 · Stabilizer Control SystemSDR DL72S982625Duct · brokenLOWER AFT BODY OVERHEAT LIGHT ON. REPLACED BLOWN DUCT UNDER APU IN KEEL BEAM.Dec 25, 1998 · N516DA · Boeing 727232 · Pneumatic Distribution SystemSDR DL72S982577Skin · corrodedFUSELAGE SKIN FS 950C-950D, STRINGER 28L : REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN WAS FOUND CORRODED AT STRINGER 28L BETWEEN FS 950C AND 950D. THE DAMAGE WAS REMOVED WITH A 6.3 BY 1.5 CUTOUT IN THS SKIN. THE CUTOUT WAS REPAIRED WITH AN EDec 11, 1998 · N516DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S982494Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM STA 1070 AT LBL 55 SEAT TRACK ATTACH POINT (MARKED). REPAIRED PER SRM 53-20-11 FIG 804A.Dec 1, 1998 · N516DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S982065Power Supply · inoperativeEMER TRACK LTS DAMAGED AT 26C. RELAMPED AND REPLACED LENS. ON TEST FOUND AFT FLOOR TRACK LTS INOP. FOUND AFT TRACK LIGHTING PWR SUPPLY BAD. REPLACED PWR SUPPLY. TEST GOOD.Oct 6, 1998 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S981737Battery Pack · dischargedAFT OVERHEAD EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK, OPS CK GOOD.Aug 22, 1998 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S980246Fitting · looseHORIZONTAL STABILIZER, RT ELEVATOR, REPAIR FOR LOOSE HINGE FITTING. THE STA 81.44 HINGE FITTING ON THE RT ELEVATOR WAS FOUND. LOOSE DURING INSPECTIONS REQUIRED PER AD 96-06-05. THE LOOSE FITTING WAS TIGHTENED PER PROCEDURES IN BAC S/B 727-55-0089 AND DOCUMEJan 28, 1998 · N516DA · Boeing 727232 · Elevator, Spar/RibSDR DL72S971350Doorframe · crackedTHE C-1 CARGO DOOR OPENING AFT FRAME AT STA 620 WAS FOUND CRACKED JUST BELOW THE CARGO FLOOR LINE. THE DAMAGE CONSISTED OF AN APPROX 3.0 CRACK IN THE WEB AND A SEVERED INBOARD CHORD. THIS AREA WAS REPAIRED WITH A DOUBLER AND STRAPS, APPROVED BY FAA/DER FORM Jun 24, 1997 · N516DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S970286Battery · dischargedLT WING AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED.Feb 16, 1997 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S962498Angle · crackedFOUND A .50 INCH CRACK NR 6 L/E SLAT COVE SKIN ATTACH ANGLE AT OUTBOARD UPSTOP PAD. REPAIRED PER M/M 57-54-0, PAR. 12.Nov 11, 1996 · N516DA · Boeing 727232 · Leading Edge DevicesSDR DL72S962497Angle · corrosionFOUND CORROSION ON LOWER ATTACH ANGLE FOR ACCESS PANEL 3448R. REPAIRED PER MM 53-30-1.Nov 11, 1996 · N516DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961212Light · missingEMERGENCY TRACK LIGHT FIXTURE MISSING. REPLACED SAME, NOW OK.May 18, 1996 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S960974Rib · crackedFOUND ON A-1 LETTER CHECK, CRACK IN NR 4 L/E SLAT NOSE RIB RADIUS OUTBOARD SIDE OF OUTBOARD TRACK. REPAIRED PER M/M 57-54-0.Apr 23, 1996 · N516DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960973Skin · crackedFOUND ON A-1 LETTER CHECK, FORWARD SERVICE DOOR SKIN CRACKED AT UPPER FORWARD CORNER .50 INCH AT 2 RIVETS. REPAIRED PER M/M 52-12-0.Apr 23, 1996 · N516DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S960972Skin · crackedFOUND ON A-1 LETTER CHECK, NR 7 SLAT COVE SKIN ATTACH ANGLE CRACKED .25 INCH AT TIA DUCT. REPAIRED PER M/M 57-54-0.Apr 23, 1996 · N516DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960326Retract Mech · out of rigAFTER TAKEOFF WITH GEAR HANDLE IN OFF POS, FELT AND HEARD LOUD THUMP 4 OR 5 TIMES AT APPROX 2 MIN INTERVALS. PROBLEM WENT AWAY WITH HANDLE IN UP POSITION. RIGGED AND ADJUSTED NOSE GEAR DOORS PER MM, OPERATION NORMAL.Feb 10, 1996 · N516DA · Boeing 727232 · Landing Gear Door Retract SectionSDR DL72S954687Spar Chord · crackedDURING SHOP VISIT, THE NR 2 MIDFLAP AFT CHORD WAS FOUND CRACKED AT CUTOUT FOR INBOARD AFT FLAP DRIVE ROD. THE CHORD WAS REPAIRED PER MM 57520.Nov 18, 1995 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S954686Spar Chord · crackedDURING SHOP VISIT, THE NR 2 MIDFLAP AFT LOWER CHORD WAS FOUND CRACKED AT INBOARD AFT FLAP TRACK. THE CHORD WAS REPAIRED PER MM 57520.Nov 18, 1995 · N516DA · Boeing 727232 · Trailing Edge Flaps
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