N11612, cancelled Mar 14, 2013
Service difficulty reports · 33
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 = 'N11612' AND deregistration_id = 'N11612-2013-03-14' 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 = 'N11612' AND deregistration_id = 'N11612-2013-03-14' 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 CALA2012041600264Uplock Sensor · faultyAFTER TAKEOFF LEFT MAIN GEAR RED LIGHT REMAINED ON. AFTER GEAR RETRACTION RED UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN BOTH UP AND OFF. FOUND LT MLG UPLOCK SENSOR AT FAULT. REF MM 32-61-00-101 R/R LT MLG UPLOCK SENSOR REF MM 32-61-21. CYCLED GESDR CALA2012032900216Flex Line · tornAFTER T/O B-SYS HYD WENT TO ZERO AND BOTH PRESSURE LOW LIGHT CAME ON. RAN QRH, RETURN TO EWR. FOUND FLEX LINE TORN. REMOVED AND REPLACED FLEX LINE REF L/P 4556125 LINE, OPS CK NORMAL. OK TO CONTINUE.SDR CALA2011050200328Fuse · blownFLT DECK EMERGENCY DOME LIGHT FAILED DURING TEST, L273. FOUND EMERGENCY BATT PWR PACK M1675 AT STA 318, F4 PICO FUSE BAD. REPLACED FUSE REF AMM 33-5151-910-817C1, OPS CHECK GOOD.SDR CALA2011030700126Skin · damagedLT UPPER FUSELAGE SKIN DAMAGED AT APPROX STA 1121 BENEATH VERTICAL STAB ATTACH ANGLE. INSTALLED REPAIR DOUBLER REF EC/RA 5331-01553.SDR CALA2011030400117Skin · dentedLARGE SHALLOW DENT RT SIDE OF FUSELAGE STARTING AT STA 362.5 AND EXTENDING TO STA 372.75 AND LOCATED BETWEEN S-18R AND S-19R. REPAIRED FUSELAGE PER ECRA 5331-01552 AND INITIATED DIP 09510 TO RE-INSPECT PER PART 2 OF ECRA 5331-01552 ON OR BEFORE THE ACCUMULATISDR CALA2011030700122Skin · crackedSUPPORT TASK: PER STEP 20.0 OF EA 5330-03736 REV B CRACK INDICATION VERIFIED IN HOLE MARKED NR 1 ON FIG 5 SHEET 2 OF WORKCARD. REPAIR ACCOMPLISHED PER ECRA 5330-04106. SEQ N959 FOR DIP INITIATED.SDR CALA2011022800111Skin · dentedSUPPORT TASK - DENT ON AFT CARGO DOOR EXTERNAL SKIN LOCATED 12 INCHES FROM FWD EDGE A/Y IS LESS THAN 30. INSTALLED REPAIR DOUBLER ON AFT CARGO EXTERNAL SKIN REF SRM 52-00-01 REPAIR 3.SDR CALA2011022400108Skin · wornSUPPORT TASK E&E DOOR HAS LARGE BLEND OUT ON SKIN EDGE. REPAIRED E&E DOOR OUT SKIN REF SRM 52-00-01 PAGE 201 TO 204 (REPAIR NR 2).SDR CALA2011021800099Plate · crackedR1 DOOR-AFT LOWER CORNER STOP FITTING IS CRACKED THROUGH HI-LOK HOLE (MARKED) SEEN FROM INTERIOR P/N 65-51674-501. INSPECT STOP FITTING AND NO CRACK WAS FOUND. HOWEVER, REINFORCING PLATE ON BACK SIDE OF FITTING WAS CRACKED. REMOVED AND REPLACED REINFORCING SDR CALA2011021800098Hinge Fitting · crackedSUPPORT TASK-L-1 DOOR FWD JAMB UPPER HINGE FITTING IS CRACKED. REMOVED & REPLACED L-1 FWD JAMB UPPER HINGE FITTING REF SRM 51-40-02.SDR CALA2011021700096Frame · crackedSUPPORT TASK - LT SIDE MAIN FRAME CRACK STA 616 AT JUST BELOW MAIN DECK FLOOR ACCOMPLISHED FRAME REPAIR ON (SEE) EA 5310-05331 OP1 STEP 24.1 THRU STEP 24.14.SDR CALA2011032400176Frame · crackedFRAME CRACKED STA 867 AT S-9R. INSTALLED REPAIR ANGLES A&B REF EA 5310-04498 REV A OP2.SDR CALA2011032400175Frame · crackedFRAME CRACKED STA 907 AT S-9L. CTN53-304-108 INSTALLED REPAIR ANGLES A&B REF EA 5310-04498 REV A.SDR CALA2011032400177Frame · crackedFRAME CRACKED STA 907 AT S-9R CTN53-304-108 INSTALLED REPAIR ANGLES A&B PER EA.5310-04498, REV-A.SDR CALA2011020900077Angle · corrodedSMALL AREAS OF LIGHT CORROSION (MARKED) ON FLOOR STRUCT. "Z" ANGLE AT R2 DOOR OPENING. REMOVED DAMAGE, FOUND OUT OF LIMITS SRM 53-60-15 FIG 101. REMOVED AND REPLACED "Z" ANGLE AT R2 DOOR SRM 51-40-02.SDR CALA2011020800072Frame · crackedFRAME IS CRACKED AT O/H BIN RAIL STA 360 S-8L. INSTALLED REPAIR DOUBLERS IN REF ECRA 5310-05351.SDR CALA2011020800071Support Bracket · crackedSUPPORT TASK - STA 482 AIR CONDITIONING SUPPORT BRACKET BTWN S-8 LT & S-9 LT I/B RIVET HOLE CRACKED. INSTALLED REPAIR ANGLES REF EA 5310-04498 REV A OP 02.SDR CALA2011020700066Frame · crackedFRAME IS CRACKED AT O/H BIN RAIL STA 400 S-8L. INSTALLED REPAIR DOUBLERS AT O/H BIN RAIL STA 400 STR 8L REF EA 5310-04498 REV A.SDR CALA0700630Frame · crackedINSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME BETWEEN STRINGER 8R AND 9R, STA 727-827. A DOUBLER AND STRAP WERE INSTALLED IAW ECRA 5310-04668, REV B.SDR CALA0700620Frame · crackedINSPECTION FOUND A . 5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 440 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.SDR CALA0700619Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 380 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.SDR CALA0700618Frame · crackedINSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 787 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.SDR CALA0700617Frame · crackedINSPECTION FOUND A 5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 867 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.SDR CALA0700616Frame · crackedINSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 827 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.SDR CALA0700615Frame · crackedINSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 787 BETWEEN STRINGERS 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.SDR CALA0700614Frame · crackedINSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 747 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.SDR CALA0700613Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 400 AROUND RIVET BELOW S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.SDR CALA0700612Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 400 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.SDR CALA0700607Fitting · crackedINSPECTION FOUND A 1.5 INCH CRACK AT DOOR FITTING FASTENER IN L-1 DOOR OPENING AFT SIDE STRUCTURAL STRAP, STA 349, S16L. A REPAIR WAS INSTALLED IAW SRM 53-10-04.SDR CALA0700606Structure · crackedINSPECTION FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE IN RT FUSELAGE INNER CHORD ABOVE WING CENTER SECTION STA 616, S17R. A STIFFENING ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158.SDR CALA0700601Angle · corrodedINSPECTION FOUND AN L-2 DOOR Z-ANGLE CORRODED AT STA 907-1006, LBL 43 TO LBL 60. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-52878.SDR CALA0700599Floorbeam · corrodedINSPECTION FOUND SURFACE CORROSION ON FLOORBEAM AT STA 986, RBL 4. A REPAIR STRAP WAS INSTALLED IAW SRM 53-60-51.SDR CALA0700598Floorbeam · corrodedINSPECTION FOUND SURFACE CORROSION ON FLOORBEAM AT STA 986, RBL 40. A REPAIR STRAP WAS INSTALLED IAW SRM 53-60-51.
Back to N11612, cancelled Mar 14, 2013