N16649, cancelled Nov 30, 2011
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 = 'N16649' AND deregistration_id = 'N16649-2011-11-30' 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 = 'N16649' AND deregistration_id = 'N16649-2011-11-30' 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 CALA2010062800307Frame · corrodedFRAME STA 767 AT S27R TO S26R HAS CORROSION. INSTALLED REPAIR PARTS ON FRAME, REPAIR 4 REF-SRM 53-00-07.SDR CALA2010062800306Frame · corrodedFRAME STA 767 AT STR 27L TO STR 28L HAS CORROSION. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED REPAIR REF SRM 53-00-07 FIG 201 REPAIR 4.SDR CALA2010062800303Hinge Fitting · crackedSUPPORT TASK CRACK INDICATION W/HFEC HOLE PROBE REF STEP 20.0 OF 5330-03736. REMOVED AND INSTALLED NEW HINGE FITTING PER SRM 51-40-01 AND 51-10-02 PARAGRAPH 8.SDR CALA2010062500301Skin · crackedSUPPORT TASK-L-1 DOOR OPENING SURROUND STRUCTURE-UPPER HINGE CUTOUT INTERNAL CASTING (FITTING) IS CRACKED APPROX .6250 INCH IN LENGTH (MARKED). REMOVED AND REPLACED L-1 DOOR UPPER HINGE CASTING REF SRM 51-40 -02.SDR CALA2010062500300Skin · crackedL-1 DOOR INNER SKIN FASTENERS CRACKED (MARKED) TASK {B737-52-4-0048}. REMOVED AND REPLACED 91 MARKED INNER SKIN FASTENERS ON L-1 DOOR REF: SRM 51-40-02.SDR CALA2010062200291Web · crackedWEB LOCATED AT BL 0 FROM STA 380-STA 400 IS CRACKED AT TOP, FWD FASTENER HOLE. INSTALLED NEW WEB AT BL 0 STA 380-400 REF SRM 51-40-02.SDR CALA2010062200290Intercostal · crackedMULT-06-3-0037 CABIN FLOOR INTERCOSTAL BETWEEN STA 380 AND STA 400 AT BL 0 IS CRACKED FASTENER HOLE. INSTALLED NEW CABIN FLOOR INTERCOSTAL BETWEEN STA 380-400 AT BL 0 REF SRM 51-40-02.SDR CALA2009082400458Megaphone · inoperativeAFT FLT ATTENDANT EMERGENCY MEGAPHONE SIREN WILL NOT TEST. REMOVED AND REPLACED THE AFT FLT ATTENDANT EMERGENCY MEGAPHONE. OPS CHECKS GOOD.SDR CALA0800963Frame · crackedFUSELAGE STATION 360 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET INBOARD RIVET BETWEEN STRINGERS 8 AND 9. REPAIRED 360 FRAME AT STR 8-9 LEFT PER ECRA 5310-04845.SDR CALA0800960Frame · crackedFUSELAGE STATION 867 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 867 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.SDR CALA0800959Frame · crackedFUSELAGE STATION 827 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 827 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA5310-044498.SDR CALA0800958Frame · crackedFUSELAGE STATION 747 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 747 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.SDR CALA0800957Frame · crackedFUSELAGE STATION 787 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 787 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.SDR CALA0800956Frame · crackedFUSELAGE STATION 867 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 867 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR ANGLES PER EA5310-04498.SDR CALA0800955Frame · crackedFUSELAGE STATION 827 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 827 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.SDR CALA0800954Frame · crackedFUSELAGE STATION 787 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 787 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.SDR CALA0800953Frame · crackedFUSELAGE STATION 747 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 747 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.SDR CALA0800952Frame · crackedFUSELAGE STATION 400 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 400 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.SDR CALA0800949Skin · delaminatedRIGHT WING NUMBER 5 SLAT TRAILING EDGE OUTBOARD END DELAMINATED. REPAIRED DELAMINATION ON OUTBOARD END OF NUMBER 5 SLAT PER B737-500 SRM 51-70-10.SDR CALA0800944Web · damagedBODY STATION 787 AT STRINGER 25R FRAME CLOSE-OUT WEB DAMAGED. REMOVED DAMAGED WEB CLOSE-OUT AT BODY STATION 787 AT STR 25R IAW B737 SRM 51-40-02, FABRICATED NEW WEB PER BOEING DRAWING 65-56655. ALODINED AND PRIMED PER B737 SRM 51-20-01. INSTALLED NEW WEB CLSDR CALA2008100600944Frame · damagedBODY STATION 787 AT STRINGER 25R FRAME CLOSE-OUT WEB DAMAGED. REMOVED DAMAGED WEB CLOSE-OUT AT BODY STATION 787 AT STR 25R IAW B737 SRM 51-40-02, FABRICATED NEW WEB PER BOEING DRAWING 65-56655. ALODINED AND PRIMED PER B737 SRM 51-20-01. INSTALLED NEW WEB CLSDR CALA0800939Frame · crackedFUSELAGE STATION 400 LEFT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGER'S 8L AND 9L. REPAIRED FRAME 400 LT PER EA 5310-04498 BETWEEN STR 8L AND 9L.SDR CALA0800943Angle · crackedAFT CARGO COMPARTMENT RIGHT FLOOR TO SIDEWALL TRANSITION ANGLE IS CRACKED AT STATION 747 AND STATION 727C. REMOVED DAMAGED SECTION OF AFT CARGO COMPARTMENT RIGHT TRANSITION ANGLE FROM STATION 747 TO STATION 727C, FABRICATED REPAIR FROM BAC1496-377 EXTRUSION PSDR CALA0800938Torque Box · corrodedL-2 DOOR TWO MOUNT HOLES ON TORQUE BOX CORRODED. REMOVED AND REPLACED L2 DOOR TORQUE BOX AS CORROSION WAS FOUND TO BE OUT OF LIMITS PER B737 CMM 52-6-03.SDR CALA0800935Intercostal · crackedFORWARD CARGO INTERCOSTAL DAMAGED BETWEEN STATIONS 380-400 AT S-22R. REPAIRED FORWARD CARGO INTERCOSTAL DAMAGED BETWEEN STATIONS 380-400 AT S-22R PER B737-500 SRM 51-70-11.SDR CALA0800925Intercostal · crackedFWD WET AREA CROSS BRACE CRACKED AT FLOORBOARD ATTACH HOLES BETWEEN STA 340-360 LBL 46. REMOVED AND REPLACED INTERCOSTAL AT LBL 46 BS 328 TO BS 344 REF 737-500 SRM 51-40-02.SDR CALA0800922Intercostal · crackedFORWARD WET AREA CROSSBRACE CRACKED AT FLOORBOARD ATTACH HOLES BETWEEN STATION 360-380 LBL 12. ORIGINAL DAMAGE WAS TO INTERCOSTAL LOCATED AT LBL 12 BETWEEN BODY STATIONS 344-360, REMOVED DAMAGE TO UPPER FLANGE OF INTERCOSTAL AT LBL 12 BETWEEN BS 344 TO BS 360SDR CALA0300694Skin · gougedAPU ACCESS DOOR INNER SKIN GOUGED LT SIDE FORWARD OF AFT LATCH. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 5200-01.SDR CALA0300685Bushing · corrodedCORROSION ON FORWARD LOWER HORIZONTAL STAB CENTER SECTION LUG ON AFT CLEVIS ON AFT FACE AT BUSHING. REMOVED AND REPLACED BUSHING PER SOPM 20-50-03.SDR CALA0300684Bushing · corrodedFORWARD LEFT LOWER HORIZONTAL STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT BUSHING ON FORWARD FACE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.SDR CALA0300683Bushing · corrodedFORWARD LEFT UPPER STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT THE BUSHING ON FORWARD EDGE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.SDR CALA0300682Bushing · corrodedCORROSION ON FORWARD UPPER HORIZONTAL STAB CENTER SECTION LUG AFT CLEVIS ON AFT FACE AT BUSHING. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.SDR CALA0300680Angle · corrodedINSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 967-990. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0300377Skin · damagedTHE FUSELAGE SKIN WAS FOUND DAMAGED AFT OF BS 1088 BETWEEN STRINGER 18L AND 20L. THE TRIM OUT TO REMOVE DAMAGE MEASURED 1.3 X 1.15 INCH. THE AREA WAS REPAIRED IAW ECRA 5330-03264.
Back to N16649, cancelled Nov 30, 2011