N15790, cancelled Nov 27, 2012
Service difficulty reports · 75
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 = 'N15790' AND deregistration_id = 'N15790-2012-11-27' 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 = 'N15790' AND deregistration_id = 'N15790-2012-11-27' 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 MZZA00013Skin · corrodedGUM - LOWER FUSELAGE APPROXIMATELY 6 O''CLOCK POSITION HAS CORROSION BUILD UP THROUGH OUT LEFT AND RIGHT FORWARD OF RAM AIR INLET. SKIN OF AIRCRAFT CORRODED AT BS 720A - 720B BETWEEN S28L AND S27R. AREA OF DEFECT DIRECTLY ABOVE RAM AIR DOOR INLET SCOOP. MAISDR MZZA00007Toggle · crackedFLT 977 - AFTER TAKEOFF, INDICATION OF LEADING EDGE FLAPS AND SLATS EXTENDED INDICATED AT CONTROL PANEL AND GREEN LIGHT MAIN FLAPS OUTBOARD INDICATION STOPPED AT 4 DEGREES, INBOARD INDICATION STOPPED AT 2 DEGREES, AILERON L-1 DEGREE, RUDDER L-2.5 DEGREES TO GESDR MZZA99127Stringer · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 5 SQUARE INCH AREA CORROSION WAS FOUND ON STRINGER 27L BETWEEN BS 720F PLUS 6 AND BS 740. THE CORRODED PART OF STRINGER WAS TRIMMED OUT AND REPAIRED PER B727 CHAP 53-10-03 FIG 1. (M)SDR MZZA99135Skin · corrodedTNN - DURING D-CHECK INSPECTION ON AIR ASIA, A 4 INCH BY 32 INCH AREA CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN BS 448 AND BS 480, STRINGER 26R. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M)SDR MZZA99123Channel · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1. 5 INCH LONG CRACK WAS FOUND ON U-CHANNEL ATTACHED TO RIGHT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 CHAPTER 51-40-03 AND 51-30-02. (M)SDR MZZA99125Splice · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH IG CORROSION WAS FOUND ON STRINGER 30 SPLICE ON CARGO COMPARTMENT AT BS 1010. THE DAMAGED PART WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAPTER 53-10-03 FIG 1. (M)SDR MZZA99118Stringer · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CRACK ON RIGHT WING UPPER VENT STRINGER 12 AND WS 686.5 WEB ATTACHMENT. THE CRACKED STRINGER WAS TRIMMED OUT AND REPAIRED PER EA 5762-01050 PART 3. (M)SDR MZZA99117Stringer · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CRACK ON RIGHT WING UPPER VENT STRINGER 11 AND WS 629 WEB ATTACHMENT. THE CRACKED STIFFENER WAS TRIMMED OUT AND REPAIRED PER EA 5762-01050 PART 3. (M)SDR MZZA99126Stringer · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH BY 32 INCH AREA CORROSION WAS FOUND ON STRINGER 26R BETWEEN BS 448 AND BS 480. THE CORRODED PART OF STRINGER WAS TRIMMED AND REPAIRED PER B727 CHAPTER 53-10-03 FIG 1. (M)SDR MZZA99112Web · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.625 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB AT BS 1213. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 51-40-02 FIG 1. (M)SDR MZZA99120Frame · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 30 SQUARE INCH AREA IG CORROSION WAS FOUND ON FUSELAGE FRAME AT BS 219 AND RT WL 233. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER SRM 51-40-03. (M)SDR MZZA99140Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH BY 4 INCH AREA IG CORROSION WAS FOUND ON PASSENGER FLOOR SEAT TRACK AT BS 395 AND RBL 40. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M)SDR MZZA99134Floorbeam · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 6 INCH AREA IG CORROSION WAS FOUND ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT BS 328 FROM LBL 01 TO RBL 05. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 51-40-04 FIG 2SDR MZZA99133Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR SEAT TRACK BETWEEN BS 360/380 ALONG RBL 18. THE DAMGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M)SDR MZZA99132Seat Track · corrodedTNN - DURING D-CHECK INSPECTON ON AIRCRAFT AT AIR ASIA, A 1 INCH BY 20 INCH AREA IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR SEAT TRACK BETWEEN BS 360 AND 380 ALONG RBL 22 AND RBL 24. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-1SDR MZZA99119Stiffener · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT WING FRONT SPAR STIFFENER AT SS 58. THE CORRODED WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M)SDR MZZA99142Frame · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.5 INCH LONG CRACK WAS FOUND ON C3 DOOR FORWARD FLANGE AT STRINGER 27R ON CARGO COMPARTMENT. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAP 53-10-04 FIG 1. (M)SDR MZZA99141Floorbeam · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH AREA IG CORROSION WAS FOUND ON BS 1148 FLOORBEAM UPPER CHORD AT LBL 10. THE CORROED PART OF UPPER WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAP 53-10-08 FIG 3. (M)SDR MZZA99128Frame · corrodedDURNIG D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH IG CORROSION WAS FOUND ON BS 1148 FRAME FORWARD FLANGE ON CARGO COMPARTMENT. THE CORRODED PART OF FRAME WAS TRIMMED OUT AND REPAIRED PER B727 CHAP 53-10-04 FIG 1. (M)SDR MZZA99122Spar Chord · corrosionTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON VERTICAL STABILIZER FRONT SPAR LEFT CHORD AT FS 54. THE CORRODED AREA IS TRIMMED OUT AND REPAIRED PER ECRA 5530-01250. ISSUE A NEW DIP NR CM 556 TO READ AS FOLLOWS WITHIN 11 MONTSDR MZZA99137Skin · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH IG CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN STRINGER 27R AND BS 720D PLUS 13. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M)SDR MZZA99129Shear Tie · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH AREA IG CORROSION WAS FOUND ON BS 950E SHEAR TIE ON CARGO COMPARTMENT. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAP 53-10-04 FIG 14. (M)SDR MZZA99124Skin · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 5 SQUARE INCH IG CORROSION WAS FOUND ON FUSELAGE SKIN AT BS 720F PLUS 4 AND STRINGER 28L - STRINGER 26R. THE CORRODED AREA WAS CLEANED UP AND REPAIRED PER EC/RA 5330-02842. (M)SDR MZZA99136Skin · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .75 INCH LONG CRACK WAS FOUND ON FUSELAGE SKIN BETWEEN STRINGER 28R AND BS 720A PLUS 4. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M)SDR MZZA99138Beam · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON RIGHT STABILIZER UPPER T/E BEAM AT ELEVATOR STATION 190. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. (M)SDR MZZA99139Beam · corrosionTNN - DURING D-CHECK INSPECTION AT AIR ASIA, A 3 INCH LONG CORROSION WAS FOUND ON LEFT STAB UPPER T/E BEAM AT ELEV STATION 119. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-06 FIG 1. (M)SDR MZZA99131Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON BS 1130 AND LBL 46 SEAT TRACK. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. (M)SDR MZZA99130Beam · corrosionTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON LEFT STABILIZER UPPER T/E BEAM AT ELEVATOR STATION 155. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. (M)SDR MZZA99121Skin · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A RIGHT VERTICAL STABILIZER SKIN WAS FOUND CRACKED JUST AFT TO THE BS 1183 BULKHEAD AT APPROX WL 302. NO ADDITIONAL REWORK OF THE CRACK IS NECESSARY DUE TO WITHIN LIMIT. ISSUE A DIP NR CM558 TO INSPECTSDR MZZA99116Web · crackTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1275. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-02 FIG 1. (M)SDR MZZA99115Channel · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.25 INCH LONG CRACK WAS FOUND ON U-CHANNEL WHICH IS ATTACHED LEFT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMAGED ANGLES WERE REMOVED AND REPLACED PER B727 SRM CHAP 51-40-03. (M)SDR MZZA99114Web · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO PLACES 1. 5 INCH AND .625 INCH LONG CRACKS WERE FOUND ON L-ANGLES WHICH ARE ATTACHED TO RGHT LOWER TORQUE BOX VERTICAL WEB AT BS 1263. THE DAMAGED ANGLES WERE REMOVED AND REPLACED PER B727 SRM CHAPTSDR MZZA99113Web · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB AT BS 1229. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 51-40-02 FIG 1. (M)SDR CALA9802145Fuse · failedINSPECTION FOUND AFT SECTION OF AISLE EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND PINS PULLED OUT OF CONNECTOR AT ROW 20 SEAT LIGHT PIGTAIL. THE CONNECTOR WAS REPINNED. ALSO, FOUND AFT POWER SUPPLY BASE F-2 FUSE BLOWN. THE FUSE WAS REMOVED AND RESDR CALA9801846Wire · brokenINSPECTION FOUND R-1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT LIGHT ASSEMBLY.SDR CALA9801845Skin · corrodedINSPECTION FOUND THE RT WING INBOARD MIDFLAP CORRODED AROUND TWO RIVETS ON UPPER SURFACE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.SDR CALA9801844Skin · corrodedINSPECTION FOUND NR 5 SPOILER CORRODED ALONG TOP EDGES. THE NR 5 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.SDR CALA9801843Skin · delaminatedINSPECTION FOUND THE NR 2 SPOILER DELAMINATED AFT OF INBOARD HINGE. THE NR 2 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.SDR CALA9801842Skin · delaminatedINSPECTION FOUND RT WING INBOARD TRAILING EDGE AFT FLAP DELAMINATED AT OUTBOARD AND INBOARD TRAILING EDGE CORNER. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.SDR CALA9801841Skin · delaminatedINSPECTION FOUND NR 7 SPOILER DELAMINATED AT LOWER OUTBOARD AFT TRAILING EDGE. THE NR 7 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.SDR CALA9801840Skin · delaminatedINSPECTION FOUND LT OUTBOARD AFT FLAP OUTBOARD LOWER CORNER DELAMINATED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-61-12.SDR CALA9801839Skin · corrodedINSPECTION FOUND NR 1 SPOILER CORRODED ALONG OUTBOARD EDGE AND DELAMINATED ON TOP. THE NR 1 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.SDR CALA9801816Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN NOSE WHEEL WELL STIFFENER AT STA 234, LBL 20. THE STIFFENER WAS REPAIRED IAW SRM 51-10-2.SDR CALA9801815Chord · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING LOWER CHORD AT NR 7 SPOILER ACTUATOR. THE CRACKED AREA WAS CUT OUT, STRAPS AND CHORD ANGLE WERE INSTALLED IAW ECRA 5720-01680 AND SRM 51-10-2.SDR CALA9801814Stiffener · corrodedINSPECTION FOUND LT WING FRONT SPAR STIFFENER CORRODED ON INBOARD SIDE CENTER AT STA 224. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2 AND 51-20-4.SDR CALA9801790Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT FS 1090 TO 1130, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.SDR CALA9801789Skin · delaminatedINSPECTION FOUND LT INBOARD AILERON TAB TRAILING EDGE SEPARATED IN TWO AREAS. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-11.SDR CALA9801788Bracket · corrodedINSPECTION FOUND NR 7 SPOILER ATTACH SUPPORT BRACKET CORRODED. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9801787Beam · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING TRAILING EDGE J-BEAM ABOVE NR 7 SPOILER ACTUATOR. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5750-02914 AND SRM 51-10-6.SDR CALA9801786Battery · dischargedINSPECTION FOUND MAIN CABIN EMERGENCY LIGHT AT ROW 8 HAD A WEAK BATTERY. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-50-00.
Back to N15790, cancelled Nov 27, 2012