N12FQ

Service difficulty reports not matched to an aircraft · 41

They name N12FQ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N12FQ' AND registry_match IS NULL
  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 DU4R05060313Panel · puncturedRT CABIN STA. 655 AND 674 PANEL B8 HAS PUNCTURES.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Structure (General)SDR DU4R05060312Panel · puncturedR/H CABIN STA. 335 PANEL B2 IS PUNCTURED.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Structure (General)SDR DU4R05060311Panel · puncturedRT CABIN STA 350.5 PANEL D2 IS PUNCTURED.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Structure (General)SDR DU4R05060310Panel · puncturedRT CABIN STA 693 PANEL D9 IS PUNCTURED.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Structure (General)SDR DU4R0506039Skin · dentedDENT AT FS 237 LEFT LONGERON 17 AND 18L .021 BY .750 IN D/X 35.7.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Main, Plate/SkinSDR DU4R0506036Threshold · corrodedAFT CARGO DOOR THRESHOLD HAS CORROSION AROUND FASTENER HOLES AT L-28R.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Miscellaneous StructureSDR DU4R0506038Skin · dentedFUSELAGE SKIN AT FS 224 L-19L 1.2 BY 1.9 IN. DENT 0.043 IN. DEPTH D/X 27.9.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Main, Plate/SkinSDR DU4R0506035Floor Panel · delaminatedLT FLOOR PANEL FS 866 BL 44.5 TO 24.5 DELAMINATED AND SOFT SPOTS.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Floor PanelSDR DU4R0506033Floor Panel · damagedCABIN FLOOR PANEL AT FS 875 - 864 HAS A SOFT SPOT LT OVER FUEL ACCESS PANEL.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Floor PanelSDR DU4R0506037Floor Support · crackedCENTER FLOORBOARD AT FS 807 TO 886 HAS CRACKED SUPPORT ANGLE.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Miscellaneous StructureSDR DU4R0506034Floorboard · damagedFLOORBOARD AT R/S SEAT TRACK STA 1193-1250 HAS SOFT SPOTS.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Floor PanelSDR DU4R0506032Seat Track · corrodedFWD CABIN 256 LBL 24 SEAT TRACK LOWER LEG IS CORRODED.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DU4R0506031Floorboard · damagedPAX CABIN FLOORBOARD BETWEEN L/S SEAT TRACK AT FS 389 - 465 HAS A VERY SOFT AND VOIDED AREA.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Floor PanelSDR 20052400AFloorbeam · corrodedCABIN FLOOR SUPPORT STRUCTURE FS 256.0 LBL 44 TO RBL 44 HAS CORROSION.Jun 3, 2005 · N12FQ · Doug MD88 · Fuselage Main, Floor BeamSDR 97Floor Support · corrodedCABIN FLOOR SUPPORT STRUCTURE FS 200.0 - 256.0 LBL 15 CORRODED.May 10, 2005 · N12FQ · Doug MD88 · Fuselage Miscellaneous StructureSDR 96Floor Support · corrodedCABIN FLOOR SUPPORT STRUCTURE FS 160 - 200 RBL 38 CORRODED.May 10, 2005 · N12FQ · Doug MD88 · Fuselage Miscellaneous StructureSDR 95Skin · dentedDENTED FUSELAGE SKIN FS 314 BETWEEN L-23L AND L-24L 2.3 X 1.4 INCH, DEPTH 0.013 INCH.May 5, 2005 · N12FQ · Doug MD88 · Fuselage Main, Plate/SkinSDR 94Skin · dentedDENTED FUSELAGE SKIN FS 740 BETWEEN L-27L AND L-28L 2.0 X 2.5 INCH DEPTH 0.075 INCH.May 5, 2005 · N12FQ · Doug MD88 · Fuselage Main, Plate/SkinSDR 93Skin · dentedDENTED FUSELAGE SKIN FS 585 BETWEEN L-23L AND L-24L 3.25 X 2.25 INCH DEPTH, 0.015 INCH.May 5, 2005 · N12FQ · Doug MD88 · Fuselage Main, Plate/SkinSDR 92Skin · dentedDENTED FUSELAGE SKIN FS 123 L-26R DEPTH 0.054, 2.30, 3.2.May 5, 2005 · N12FQ · Doug MD88 · Fuselage Main, Plate/SkinSDR 91Floor Panel · delaminatedDELAMINATED LEFT STA 160 - 200 FLOOR PANEL WITH HOLES AND MISSING INSERTS.May 5, 2005 · N12FQ · Doug MD88 · Fuselage Floor PanelSDR 90Web · puncturedPUNCTURED CABIN FLOOR WEB FS 170.0 LBL-44.May 5, 2005 · N12FQ · Doug MD88 · Fuselage Miscellaneous StructureSDR 88Web · corrodedCORRODED CABIN FLOOR WEB BS 180.0 RBL-0-36.May 5, 2005 · N12FQ · Doug MD88 · Fuselage Miscellaneous StructureSDR 87Floor Support · corrodedCORRODED CABIN FLOOR SUPPORT STRUCTURE FS 180.0 RBL 0-36.May 5, 2005 · N12FQ · Doug MD88 · Fuselage Miscellaneous StructureSDR 86Floor Support · corrodedCORRODED CABIN FLOOR SUPPORT STRUCTURE FS 2092.0 RBL-11.May 5, 2005 · N12FQ · Doug MD88 · Fuselage Miscellaneous StructureSDR A4JA12100401Connector · looseAT CRUISE ALTITUDE, THE AFT CARGO B FAIL LIGHT ILLUMINATED ON THE CARGO FIRE DETECTION PANEL. FOUND CONNECTOR LOOSE, RESECURED IAW MM 20-50-04. OPS CHECK OK.Nov 26, 2004 · N12FQ · Doug MD88 · Fire DetectionSDR 04232004SO35Valve · failedDURING INITIAL CLIMB SMOKE ENTERED COCKPIT AND REAR PORTION OF CABIN.TROUBLE SHOT AND FOUND LEFT HAND TEMP CONTROL VALVE STUCK OPEN TO FULL HOT. REMOVED AND REPLACED LEFT HAND TEMP CONTROL VALVE IAW MD80 MM 21-61-01. OPERATIONAL AND LEAK CHECKS GOOD.AS A PRECAApr 22, 2004 · N12FQ · Doug MD88 · Cabin Temperature ControllerSDR 2003F00371Smoke Detector · will not testDURING A-CHECK, FOUND RIGHT AFT LAVATORY SMOKE DETECTOR DOES NOT TEST. REPLACED RIGHT AFT LAVATORY SMOKE DETECTOR IAW MM 26-14-00. CHECK NORMAL. (M)Apr 2, 2003 · N12FQ · Doug MD88 · Smoke DetectionSDR 2003F00043Valve · malfunctionedAFTER DEPARTURE FROM PIE-20 MINUTE INTO FLIGHT TO SFB, THE CREW GOT A TAILCONE OVERHEAT LIGHT AND DID A RETURN TO FIELD PIE. REMOVED AND INSTALLED AUGMENTATION VALVE IAW MD80 MM 36-10-01. OPS CHECK GOOD IAW MD80 MM 36-10-00. (M)Sep 16, 2002 · N12FQ · Doug MD88 · Pneumatic Distribution SystemSDR A4J2002F00003Valve · inoperativeAFTER DEPARTURE, 20 MINUTES INTO FLIGHT, THE CREW GOT A TAILCONE OVERHEAT LIGHT AND DID A RETURN TO FIELD. REMOVED AND INSTALLED AUGMENTATION VALVE IAW MM. OCK GOOD IAW MM.Sep 16, 2002 · N12FQ · Doug MD88 · Pneumatic Distribution SystemSDR 2003F00042Sense Line · blockedUPON ENGAGING AUTO THROTTLE THE LEFT ENGINE WOULD NOT SPEED TO TAKEOFF POWER. FOUND TWO B-NUTS ON NR 1 ENGINE PT-2 LINE AND BOTH P2-2 LINES ON NR 1 AND NR 2 ENGINE BLOCKED. CLEARED BLOCKAGE AND TIGHTENED B-NUTS, OPS CHECK OK ON ENGINE RUN IAW MD80 MM 71-11-0Sep 8, 2002 · N12FQ · Doug MD88 · Fuel Controlling SystemSDR A4J2002F00002Line · blockedUPON ENGAGING THROTTLE THE LT ENGINE WOULD NOT SPEED TO TAKEOFF POWER. BOTH PT2 LINES ON NR 1 AND NR 2 ENGINE BLOCKED. CLEARED BLOCKAGE AND CHECKED BNUT CONNECTIONS, OCK, OK ON ENGINE RUN IAW MM. ALSO TRIMMED NR 1 AND NR 2 ENGINE., AND OCK, IAW MM.Sep 8, 2002 · N12FQ · Doug MD88 · Engine Pressure Ratio (EPR)SDR 2003F00041Sleeve · tornTAIL COMPARTMENT, HOT LIGHT CAME ON JUST AFTER TAKEOFF. FOUND TORN SLEEVE ON DUCT. REMOVED AND REPLACED DUCT SLEEVE IAW MD80 MM CHAPTER 20-10-11. OPS AND LEAK CHECK GOOD IAW MD 80 MM CHAPTER 21-20-00. (M)Sep 5, 2002 · N12FQ · Doug MD88 · Air Distribution SystemSDR A4J2002F00005Sleeve · tornTAIL COMPARTMENT, HOT LIGHT CAME ON JUST AFTER TAKEOFF. FOUND TORN SLEEVE ON DUCT. REMOVED AND REPLACED DUCT SLEEVE IAW MM. OPS AND LEAK CHECK GOOD, IAW MM.Sep 5, 2002 · N12FQ · Doug MD88 · Air Distribution SystemSDR ERKR200100070Panel · corrodedREPAIR- CORROSION, LEFT LOWER FORWARD WING PANEL, XFS=129.847. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR CORROSION FOUND COMMON TO THE LOWER SURFACE OF THE LEFT WING FORWARD PANEL, (P/N 9937581-505). REPAIR IS ACCOMPLISHED BY BLENDING OUT THE CORROSION Mar 26, 2001 · N12FQ · Doug MD88 · Wing, Plate/SkinSDR ERKR200100069Hinge · corrodedREPAIR - CORROSION, HORIZONTAL STABILIZER HINGE - SIDE LOAD FITTING. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR CORROSION FOUND AT THE HORIZONTAL STABILIZER HINGE SIDE LOAD FITTING. THE CORROSION IS IN THE AREA OF THE 2.0 INCHES DIAMETER COUNTERBORE. THMar 26, 2001 · N12FQ · Doug MD88 · Horizontal Stabilizer StructureSDR ERKR200100067Skin · damagedREPAIRED SKIN PANEL, STATION 560, STRINGER 24R-25R RIGHT.Mar 26, 2001 · N12FQ · Doug MD88 · Fuselage Main, Plate/SkinSDR ERKR20010068Skin · corrodedRIGHT HORIZONTAL STABILIZER, BARREL NUT HOLES XHS 27.234. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR CORROSION FOUND IN THE THREE BARREL NUT HOLE BORES OF THE RIGHT HORIZONTAL STABILIZER LOWER FORWARD AND LOWER CENTER SKIN PANELS. PART NUMBERS 5922576504 AMar 26, 2001 · N12FQ · Doug MD88 · Horizontal Stabilizer, Plate/SkinSDR ERKR200100065Skin · damagedREPAIR-SKIN PANEL, STATION 560, STRINGER 27 RIGHT. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR REPLACEMENT OF AN EXISTING REPAIR WITH A PERMANENT REPAIR AT THE SUBJECT LOCATION. THE SKIN PANEL WAS FOUND TO HAVE AN UNDOCUMENTED REPAIR IN THE AREA OF AN INTMar 26, 2001 · N12FQ · Doug MD88 · Fuselage Main, Plate/SkinSDR ERKR200100066Skin · dentedDENTED SKIN AT STATION 540 - 560, BETWEEN L17 AND L18 RIGHT HAND SIDE. ADDRESS REPAIR OF EXISTING DENTED SKIN LOCATED AT STATION 540 - 560, BETWEEN L17-L18, RIGHT HAND SIDE PER ECRA N12FQ-53-MD88-009-EAC.Mar 26, 2001 · N12FQ · Doug MD88 · Fuselage Main, Plate/SkinSDR 96ZZZX6127Duct · b nut looseAFTER TAKEOFF, PILOT REPORTED NR 2 ENGINE OVERHEAT LIGHTS CAME ON ONE AFTER THE OTHER. AIRCRAFT LEVELED OFF. NR 2 THROTTLE RETARDED AND OVERHEAT CONDITION DISAPPEARED. AIRCRAFT RETURNED TO DEPARTING AIRPORT AND NORMAL LANDING PERFORMED. INSPECTION REVEALEDOct 13, 1996 · N12FQ · Doug MD88 · Engine Anti-Icing System
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