N76752, cancelled Sep 25, 2006
Service difficulty reports · 97
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 = 'N76752' AND deregistration_id = 'N76752-2006-09-25' 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.
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 = 'N76752' AND deregistration_id = 'N76752-2006-09-25' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR XN0A1329Start Valve · malfunctionedON PUSHBACK AT PHL COULD NOT GET NR 1 START VALVE TO OPEN ELECTRICALLY. COULD NOT DUPLICATE, OPERATED NR 1 START VALVE NUMEROUS TIMES, SYSTEM OPS CHECK GOOD IAW B727 MM CHAPTER 80-11-11. DMI 6492 CLEARED.SDR XN0A1320Brake Assy · draggingON TAXI OUT AIRCRAFT BRAKES SEEMED TO DRAG, AIRCRAFT CAME TO A STOP. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW B727 MM CHAPTER 32-41-32. REMOVED AND REPLACED NR 1 MLG WHEEL ASSY IAW B727 MM CHAPTER 32-45-01, OPS CHECKS AND LEAKS GOOD.SDR XN0A1920Brake Assy · draggingON TAXI OUT AIRCRAFT BRAKES SEEMED TO DRAG, AIRCRAFT CAME TO A STOP. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW B727 MM CHAPTER 32-41-32. REMOVED AND REPLACED NR 1 MLG WHEEL ASSY IAW B727 MM CHAPTER 32-45-01, OPS CHECKS AND LEAKS GOOD.SDR XN0A1284Switch · inoperativeAMBER LE LIGHT ON WITH FLAPS SET TO 15 DEGREES. NR 6 LE SLAT DOES NOT INDICATE EXTEND. REPLACED NR 6 SLAT POSITION INDICATING SWITCH. OPS CHECKS GOOD IAW MM CHAPTER 27-82-11.(STATUS:SUPP/CLOSED).SDR XN0A1263Cabin Pressure · malfunctionedAIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE - AUTO, STANDBY OR MANUAL AC OR DC. TRANSFERRED TO MEL 5718 IAW MEL 21-16-2D. PLACARDS INSTALLED CAT-C.SDR XN0A1254Brake Assy · vibratesON TAXIOUT, BRAKES VIBRATE WHEN APPLIED. BLED BRAKES AS REQ'D IAW B727 MM REF 32-41-0, SYSTEM OPS CHECKS GOOD.SDR XN0A1253Exciter · failedON ENGINE START NR 2 ENGINE WOULD NOT START, START VALVE OPENS PRESSURE DROP NO EGT. REMOVED AND REPLACED NR 2 ENG EXCITER BOX IAW MM 74-11-1, OPS GOOD.SDR XN0A1236Warning Light · illuminatedDURING EMERGENCY DESCENT, LT DUCT OVERHEAT LIGHT TRIP, PERFORMED ALL CHECKLIST.SDR XN0A1235Ignition Unit · malfunctionedNR 2 ENGINE WILL NOT START, NO IGNITION. NR 2 ENGINE IGNITION CB'S RESET, OP'S CHECK GOOD.SDR XNOA1225Engine · inoperativeNR 2 ENGINE WILL NOT START, NO IGNITION. NR 2 ENGINE IGNITION CB'S RESET, OP'S CHECK GOOD.SDR XNOA1231Selector Switch · burned outAFTER STARTING NR 3 ENGINE, AC FREQUENCY METER PEGGED OUT AND SMOKE POURED OUT OF FREQ (AC) SELECTOR SWITCH. REMOVED AND REPLACED AC FREQ METER SELECTOR SWITCH AND OPS CHECK OKAY IAW B727 MM 24-20-00.SDR XN0A1227Warning Light · illuminatedNR 3 ENGINE CSD LOW PRESSURE WARNING LIGHT ON WITH NO FREG. DISCONNECTED NR 3 CSD DEFERRED NR 3 GENERATOR INOP IAW ENA B727 MEL 24-1 PROCEDURES DMI 4858 CAT-B ITEM. PLACARDS INSTALLED.SDR XNOA1183Switch · out of adjustDURING CLIMB, MAIN CARGO DOOR LIGHT ILLUMINATED. ADJUSTED DOOR CLOSED SWITCH IAW HAMILTON-TIMCO SUPPLEMENTAL MM 7-11-1. OPS CHECKS GOOD IAW HAMILTON TIMCO-SUPPLEMENTAL MM 4.1.1SDR XNOA1179Engine · malfunctionedNR 2 ENGINE WILL NOT ACHIEVE TAKE-OFF POWER. PERFORMED NR 2 ENGINE RUN. NR 2 ENGINE MAKES ITS TARGET POWER IAW P&W JT8D MM 72-00-00. NO DEFECTS NOTED. (STATUS: ORIG/CLOSED)SDR CALA9801670Hyd Line · leakingTHE A HYDRAULIC SYSTEM WAS LOST ON FINAL APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE A SYSTEM HYDRAULIC PRESSURE LINE IN AFT AIRSTAIRS TO FIREWALL LEAKING. THE HYDRAULIC PRESSURE LINE WAS REMOVED AND REPLACED. TSDR CALA9800736Hyd Line · leakingLOSS OF A-SYSTEM HYDRAULIC FLUID UPON RETRACTING THE LANDING GEAR. REMOVED AND REPLACED TAIL SKID RIGHT HYDRAULIC LINE PER MM 32-71-12.SDR CALA9800138Bulkhead · crackedINSPECTION FOUND, A 1 CRACK IN FORWARD FACE OF STA 1183 BULKHEAD ON RT SIDE ABOVE OUTFLOW VALVE. A WEB REPAIR WAS INSTALLED IAW BOEING DRAWING NR 65C31446, SRM 51-30-0, AND ECRA 553A0022.SDR CALA9800129Battery Pack · dischargedINSPECTION FOUND, THE AFT ENTRY EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED.SDR CALA9800128Rib · crackedINSPECTION FOUND A 2 INCH CRACK AT FASTENER OF RT WING LEADING EDGE RIB, INBOARD OF NR 4 LEADING EDGE FLAP, AT L/E STA 130. THE CRACKED AREA WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9800127Skin · crackedINSPECTION FOUND A .5, 1, AND 2 CRACK IN RT SIDE OF VERTICAL STABILIZER SKIN LOWER SECTION AT STA 1343. THE AREA WAS REPAIRED IAW ECRA 5530-01190.SDR CALA9800126Stop · crackedINSPECTION FOUND A 1 CRACK IN L-1 AFT UPPER DOOR STOP AT FITTING. THE L-1 AFT UPPER DOOR STOP WAS REMOVED AND REPLACED IAW SRM 52-40-1.SDR CALA9800105Rib · crackedINSPECTION FOUND A 2 INCH CRACK AT FASTENER IN RT WING RIB INBOARD OF NR 4 LEADING EDGE FLAP AT L/E STA 130. THE CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9800078Bracket · crackedINSPECTION FOUND A .2812 INCH CRACK OUTBOARD OF NR 8 SPOILER ACTUATOR IN RT WING INBOARD TRAILING EDGE PANEL SUPPORT BRACKET AT WS 232. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND ECRA 5750-0287SDR CALA9800077Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE LOWER SKIN ABOVE NR 5 LEADING EDGE FLAP ACTUATOR, WS 224. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9800076Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN FRAME TO FUSELAGE ATTACH ANGLE IN AFT STAIR COMPARTMENT, RT SIDE, STA 1283. THE ANGLE WAS REMOVED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9800075Light · inoperativeINSPECTION FOUND EMERGENCY FLOOD LIGHT AT LEFT SIDE OVER AFT AIRSTAIRS INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED.SDR CALA9800073Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF NR 6 LEADING EDGE SLAT STA 234. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-3.SDR CALA9800072Rib · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN ABOVE PNEUMATIC DUCT FORWARD SUPPORT BRACKET AT FSS 106.8. A REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR CALA9800071Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING LEADING EDGE SKIN AT NR 6 SLAT OUTBOARD HOOK. THE CRACK WAS STOP DRILLED PER SRM 51-10-1, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4.SDR CALA9800070Skin · bentINSPECTION FOUND LT WING OUTBOARD AILERON TAB LOWER LEADING EDGE SKIN BENT AND DEBONDED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41.SDR CALA9800067Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER STRINGER NR 9 BETWEEN RIB NR 7 AND NR 8. THE CRACK WAS LOCATED AT ATTACH BOLT. THE FASTENERS WERE REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-2.SDR CALA9800066Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER STRINGER NR 8 BETWEEN RIB NR 8 AND NR 9. THE FASTENERS WERE REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-2.SDR CALA9800064Stringer · crackedINSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN LT WING SECOND UPPER STRINGER FROM REAR SPAR ABOVE RIB AT WS 629. THE FASTENERS AND CLAMPS WERE REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW EA 5762-01SDR CALA9800063Stringer · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING STRINGER AT WS 656.5, TOP OF RIB ATTACH POINT ACCESS THROUGH PANEL 7617. THE CRACK WAS STOP DRILLED AND THE AREA WAS REPAIRED IAW EA 5762-01050.SDR CALA9800062Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN LOWER EDGE AT FSS 106.8. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR CALA9800061Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB INBOARD OF NR 4 LEADING EDGE FLAP AT LEADING EGDE STA 130. THE CRACK WAS STOP DRILLED AND AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-1, AND 51-30-2.SDR CALA9800060Skin · crackedINSPECTION FOUND FOUR .5 INCH CRACKS AROUND FASTENERS OUTBOARD OF LAMP LIGHT IN WING LEADING EDGE INTERNAL SKIN AT FSS 106. THE CRACKED AREAS WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-10-6.SDR CALA9800059Rib · crackedINSPECTION FOUND A .5 INCH CRACK INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STA 130 ABOVE HOT AIR DUCT PLENUM. ALSO, A .5 INCH CRACK WAS FOUND INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STATION 130 BELOW LIGHTENING HOLE AREA. DOUBLER REPAIRS WERE FSDR CALA9800058Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN LEADING EDGE SKIN AT DOUBLER STRAP INSIDE LT WING DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR AT WS 224. THE CRACKED DOUBLER WAS REMOVED, A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9800057Stringer · crackedINSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN LT WING FIRST UPPER STRINGER FROM REAR SPAR, ABOVE RIB AT WS 656.50. THE FASTENERS AND CLAMPS WERE REMOVED. THE CRACK WAS STOP DRILLED AND THE AREA WAS REPAIRED IAW EA 5762-01050.SDR CALA9800056Skin · crackedINSPECTION FOUND A .25 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE SKIN AT AFT END OF CUTOUT WHERE NR 4 SLAT OUTBOARD HOOK ATTACHES. A DOUBLER WAS INSTALLED IAW SRM 57-30-4.SDR CALA9800055Skin · crackedINSPECTION FOUND A .25 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE SKIN AT AFT END OF CUTOUT WHERE NR 3 SLAT INBOARD HOOK ATTACHES. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4.SDR CALA9800054Skin · corrodedINSPECTION FOUND LT WING INBOARD MIDFLAP SKIN CORRODED OUTBOARD OF INBOARD CARRIAGE MOUNT AREA. A SKIN REPAIR WAS INSTALLED IAW SRM 57-50-4.SDR CALA9800053Brackets · crackedINSPECTION FOUND A .5 INCH CRACK IN INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR MOUNTS. NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1.SDR CALA9800052Brackets · crackedINSPECTION FOUND A .5 INCH CRACK IN INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 1 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-10-1.SDR CALA9800051Gusset · crackedINSPECTION FOUND A .5 INCH CRACK AT TOP CORNER AND A .5 INCH CRACK AT LOWER CORNER OF GUSSET ON RT SIDE OF VERTICAL STABILIZER AT STRINGER 9 BETWEEN RIB NR 6 AND NR 7. THE GUSSET PLATE WAS REMOVED, A NEW GUSSET PLATE WAS FABRICATED AND INSTALLED IAW SRM 55-30SDR CALA9800050Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 996, RBL 36. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6.SDR CALA9800049Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN STRINGER 15L AND 15R AT STA 720B. THE CRACKED AREAS WERE CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5.SDR CALA9800048Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN END OF STRINGER 15L AT STA 720C. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5.SDR CALA9800047Doubler · crackedINSPECTION FOUND THREE CRACKS AT HI-LOKS ON DOUBLER UPPER SIDE OF CARGO DOOR FRAME CUTOUT BETWEEN FS 604 TO 608, STRINGER 10R. THE CRACKS WERE .25 TO 1 INCH LONG. THE FASTENERS AND DOUBLER WERE REMOVED. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-
Back to N76752, cancelled Sep 25, 2006