N797AL

Service difficulty reports · 34

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 = 'N797AL' AND registry_match = 'registration'
  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 RRXA001042Transponder · failedNR 1 TRANSPONDER INOP. NR 2 TRANSPONDER INOP. NR 1 PREVIOUSLY DEFERRED SEE LP 9230-04. CLOSING ACTION REMOVED AND REPLACED TRANSPONDER SYS FUNCTIONAL TEST OK BY AVIONIC SVC RO A97A0017 USING IFR ATC-600A29 GROUND TEST SET PER MM 34-53-0. THIS CLEARS DMI C9Aug 9, 2000 · N797AL · Doug DC863 · ATC Transponder SystemSDR RRXA000235Engine · malfunctionedON TAKEOFF AT KBRO (TEMP 23C, FIELD ELE 23 FT, ANTI-ICE OFF, MAX PWR, 1.87 EPR) NR 1 ENG EGT EXCEEDED 600 CELSIUS (APPROX 610 CELSIUS FOR 5 SECONDS) AFTER LIFT OFF. POWER HAD TO BE REDUCED TO 1.70 EPR TO MAINTAIN EGT WITHIN LIMITS. SHUT ENG DOWN AS PER GOM Apr 15, 2000 · N797AL · Doug DC863 · Engine (Turbine/Turboprop)SDR RRXA991154Switch · out of adjustPASSING FL 10.0 AT DIFF PRESS 4 PSI MAIN CARGO DOOR WARNING LIGHT IN THE COCKPIT AND BY THE DOOR ILLUMINATED DEPRESSURIZED THE CABIN AT 2 1/2 DIFF PRESS WARNING LIGHT GOES OUT. ADJUSTED CARGO DOOR CLOSED SWITCH AND ADJUSTED TENSION ON GANG BAR IAW ROSENBALM AJun 23, 1999 · N797AL · Doug DC863 · Door Warning SystemSDR RRXA991139Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT W/W OVERHEAD O/B SIDE STUB FITTING AT LONGERON 24 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-0 PG 43/44.Jan 29, 1999 · N797AL · Doug DC863 · Wing, Fuselage Attach FittingsSDR RRXA991150Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOORBEAM LOWER ATTACHING CHORD AT STA 1727, BETWEEN BL 24 RIGHT AND BL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ATTACHINGJan 26, 1999 · N797AL · Doug DC863 · Fuselage Main, Floor BeamSDR RRXA991137Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON, AFT CARGO COMPARTMENT, LONGERON 34 RIGHT, BETWEEN STA 1228 AND STA 1292, UNDERNEATH DOOR THRESHOLD PLATE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. Jan 8, 1999 · N797AL · Doug DC863 · Fuselage Main, Longeron/StringerSDR RRXA991151Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1380 AND STA 1440 AT BL 59 LEFT, WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTIOJan 6, 1999 · N797AL · Doug DC863 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991149Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1280 AND STA 1300 AT BL 44 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW Jan 6, 1999 · N797AL · Doug DC863 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991148Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1280 AND STA 1300 AT BL 59 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW Jan 6, 1999 · N797AL · Doug DC863 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991147Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1300 AND STA 1320, BL 44 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW DCJan 6, 1999 · N797AL · Doug DC863 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991146Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1180 AND STA 1200 AT BL 59 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW Jan 6, 1999 · N797AL · Doug DC863 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991145Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1300 AND STA 1360 AT BL 59 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IJan 6, 1999 · N797AL · Doug DC863 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991144Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 920 AND STA 960, BL 59 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW SEAT TRACK SECTION AND INSTALLED IAW DC8 Jan 6, 1999 · N797AL · Doug DC863 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991142Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, BRACKET, CABIN FLOOR TRACK BRACKET BETWEEN STA 620 AND STA 660 AT BL 59 LEFT, WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SJan 6, 1999 · N797AL · Doug DC863 · Fuselage Miscellaneous StructureSDR RRXA991143Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 480 AND STA 520, BL 44 LEFT, WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW SEAT TRACK SECTION AND INSTALLED SEAJan 5, 1999 · N797AL · Doug DC863 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991152Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK AT BL 44 LEFT, BETWEEN STA 240 AND STA 329. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).Jan 4, 1999 · N797AL · Doug DC863 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991141Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FLOORBEAM, AT LIGHTING HOLE, STA 1702, BL 24 RIGHT, WL -6. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW FAA APPROVED COMMODORE DER ENGIJan 4, 1999 · N797AL · Doug DC863 · Fuselage Main, Floor BeamSDR RRXA991140Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FLOORBEAM, AT STA 1700, BL 20 LEFT, WL -2. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-0 AND 51-1-20D. (CORROSION DAMAGE RECORDJan 4, 1999 · N797AL · Doug DC863 · Fuselage Main, Floor BeamSDR RRXA991136Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN AT APPROX STA 1680, BETWEEN LONGERON 18 LEFT TO LONGERON 18 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLJan 2, 1999 · N797AL · Doug DC863 · Fuselage Main, Plate/SkinSDR RRXA991138Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WHEEL WELL PRESS DECK SKIN FROM FS 980 TO FS 960 AND I/B FIST HAT SECTION STIFFENER AND AROUND FITTING AT FS 960, BETWEEN LONGERON 24 LEFT AND CEILING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREAJan 1, 1999 · N797AL · Doug DC863 · Wing, Plate/SkinSDR RRXA98066Bus Power Light · illuminatedEN ROUTE, NR 1 ELECTRICAL BUSS POWER FAIL LIGHT ILLUMINATED, NR 1 BUSS DEFERRED TO KDEN. RESET NR1 BUSS, PERFORMED ENG RUN ON ALL 4 ENGS UNDER VARIOUS ELECTRICAL LOADS, SYS OPS CK GOOD.Mar 6, 1998 · N797AL · Doug DC863 · AC Power Distribution SystemSDR RRXA97220Fire Loop · malfunctionedNR 3 FIRE WARNING ON CLIMBOUT. SHUT DOWN ENGINE PER QRH. DISCHARGED BOTH FIRE BOTTLES. REMOVED AND REPLACED THE NR 3 ENGINE FWD AND AFT UPPER FIRE LOOPS, GROUND CHECKS NORMAL.Aug 14, 1997 · N797AL · Doug DC863 · Fire DetectionSDR RRXA97069Engine · oil leakWHILE EN ROUTE, CAPTAIN CALLED INTO EWA DISPATCH STATING THAT HE SHUT DOWN NR 3 ENGINE DUE TO LOW OIL QUANTITY INDICATOR. AS A RESULT, IT WAS DECIDED TO DIVERT TO IAH, WHERE EWA MECHANICS ARE ON HAND TO ASSESS DAMAGE. PERFORMED PRECAUTIONARY SHUT DOWN ON NR Mar 4, 1997 · N797AL · Doug DC863F · Turbine Engine Oil SystemSDR RRXA97025Ballast · failedCO-PILOTS GLARESHIELD FLUORESCENT TUBE BURNED OUT FOLLOWED BY A STRONG ELECTRICAL ODOR. PULLED THE INSTRUMENT PANEL C/B SMELL WENT AWAY. SUSPECT BALLAST LOCATED BY CO-PILOTS RIGHT FOOT. REMOVED AND REPLACED LIGHT TRANSFORMER BALLAST, GLARESHIELD FLUORESCENTFeb 6, 1997 · N797AL · Doug DC863 · Flight Compartment LightingSDR RRXA96085Fire Loop · dirtyCYQX - FLT DX3 - ON CLIMB-OUT AT INITIAL POWER REDUCTION, NR 3 FIRE WARNING ILLUMINATED, ENGINE PARAMETERS APPEARED NORMAL. SHUTDOWN ENGINE IAW DC-8 QRH. CLEANED LOWER FIRE LOOP AS PRECAUTIONARY. INSPECTED ENGINE FOR LEAKS, NO DEFECTS NOTED. PERFORMED HIGHSep 11, 1996 · N797AL · Doug DC863 · Fire DetectionSDR RRXA96068Air Distr · odorKDEN - FLT 110 - FUMES COME FROM CABIN AIR WHEN WARM SELECTED MANUALLY, COLD SELECTION OK, (DMI NR 608227 DEFERS AUTO CONTROL OF TEMP). RAN ENGINE OPERATED SYSTEM PER MM CHAPTER 21-00 IN WARM AND COLD POSITIONS MANUALLY. COULD NOT DUPLICATED ANY FUMES ON GROAug 28, 1996 · N797AL · Doug DC863 · Air Distribution SystemSDR RRXA96015Panel · damagedKMCN - DURING C-CHECK, FOUND UPPER ACCESS PANEL 505C HAD ATTACH SCREW HOLE DAMAGE RIGHT WING. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED BUSHING AND INSTALLED IAW DER APPROVED COTNEY ENGINEERING SKETCH A27-R01. (M)Mar 12, 1996 · N797AL · Doug DC863 · Wing, Plate/SkinSDR RRXA96014Fitting · crackedKMCN - DURING C-CHECK, FOUND FLOOR BEAM TO CUSP ATTACH BRACKET CRACKED AT FS 1220, RIGHT SIDE. MAINTENANCE REMOVED AND FABRICATED NEW FITTING IAW DER APPROVED COTNEY ENGINEERING SKETCH A27-D01. INSTALLED IAW DC8-SRM 53-1-0. (M)Mar 12, 1996 · N797AL · Doug DC863 · Fuselage Miscellaneous StructureSDR 95ZZZM245Fire Loop · disconnectedFLT 010 - KDAY-KSJC - ON CLIMB-OUT PASSING FL 240 NR 3 ENGINE FIRE LIGHT ILLUMINATED AND FIRE BELL SOUNDED. NR 3 PNEUMATIC SWITCH WAS TURNED OFF WITH NO CHANGE. ALL OTHER INDICATIONS NORMAL. SHUT ENGINE DOWN PER ENGINE FIRE CHECK LIST. LIGHT AND BELL WENT OJul 8, 1995 · N797AL · Doug DC863 · Fire DetectionSDR 95ZZZX3380Indicator Light · malfunctionedKDAY/KSJC - FLT 110 - RED DOOR NOT LATCHED LIGHT STAYED ON AFTER LANDING GEAR WAS RETRACTED. CYCLED THE GEAR AND LIGHT EXTINGUISHED. KSJC MAINTENANCE CHECKED DOOR LATCHES AND STRIKERS. CYCLED DOORS AND LATCHES INDICATION LIGHTS OPS CHECK NORMAL.Jun 14, 1995 · N797AL · Doug DC863 · Landing Gear Position and WarningSDR 95ZZZX3378Actuator · corrodedKSJC/KDAY - FLT 009 - DURING TAXI FOR DEPARTURE FROM KSJC, HAD FLAP ASSEMETRY INDICATION. CONFIRMED BY GROUND CREW OBSERVATION AT DEPARTURE END OF RUNWAY. RETURNED TO RAMP. MAINTENANCE FOUND EYEBOLT PULLED OUT FROM MID-FLAP ACTUATOR PISTON. REMOVED AND REPJun 14, 1995 · N797AL · Doug DC863 · Trailing Edge Flap ActuatorSDR 95ZZZX3174Uplatch · lack of lubeKLRD/KDAY - FLT 529 - THE MLG DOOR NOT LATCHED LIGHT REMAINED ON AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE LIGHT EXTINGUISHED NORMALLY. MAINTENANCE CLEANED AND LUBED THE UPLATCH OVER-CENTER MECHANISM. AN OPERATIONAL CHECK OF THEMay 23, 1995 · N797AL · Doug DC863 · Landing Gear Door Retract SectionSDR 95ZZZW655Hydraulic Line · damagedFLT 009 - KSJC-DAY - DURING CRUISE AT FL 330 HYDRAULIC PRESSURE FLUCTUATED ERRATICALLY FOLLOWED BY FLIGHT CONTROLS TO MANUAL REVERSION. ACCOMPLISHED HYD EMERGENCY CHECK LIST. DURING DESCENT PASSING THROUGH FL 150 PRESSURE DROPPED TO '0' AFTER 5 MINUTES. COMApr 15, 1995 · N797AL · Doug DC863 · Hydraulic System, MainSDR 95ZZZX1858Uplatch · lack of lubeKBDL/KDAY - FLT 111 - ON CLIMB-OUT FROM KBDL, GEAR UPLATCH CHECK FAILED. DOORS NOT LATCHED LIGHT REMAINED ON. CYCLED GEAR SEVERAL TIMES AND THE LIGHT EXTINGUISHED. MAINTENANCE CLEANED AND LUBED THE RT GEAR DOOR FLIGHT LOCK AND GEAR UPLATCH. ALL GEAR INDICAMar 29, 1995 · N797AL · Doug DC863 · Landing Gear Retraction/Extension System
Back to N797AL