Boeing 747-269B
Service difficulty reports · 160
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '747269B' 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 aircraft_model_key = '747269B' 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 CKSA97326Skin · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 3 PYLON SKIN CRACKED AT PNL 473EL CUTOUT. REPAIRED CRACKED SKIN IAW B747 SRM 54-30-03, (2024-T3). C CHECK WORK CARD NUMBER 7CI4709. NON-ROUTINE TASK CARD NUMBER 107894.SDR CKSA97325Skin · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 3 PYLON SKIN CRACKED AT PNL 473GL CUTOUT. REPAIRED CRACK IN SKIN IAW B747 SRM 54-30-03, (2024-T3). C CHECK WORK CARD NUMBER 7CI4709. NON-ROUTINE TASK CARD NUMBER 107893.SDR CKSA97324Chafe Strip · damagedDURING C1-12 CHECK INSPECTION, FOUND NR 4 PYLON I/B LWR SKIN AND INNER CHAFE STRIP DAMAGED FWD AND AFT OF AFT ENG MOUNT. REPAIRED DAMAGE SKIN AREA IAW B747 SRM 54-30-03. REPLACED CHAFE STRIP IAW SRM 51-10-01, 54-30-02 AND 51-30-02, (2024-T3). C CHECK WORK CSDR CKSA97323Fitting · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 4 PYLON ADP O/B MOUNTING LUG FITTING CRACKED. REMOVED AND REPLACED PART IAW B747 SRM 51-10-1 AND 51-30-02 (7075-T6). C CHECK WORK CARD NUMBER 7CI4809. NON-ROUTINE TASK CARD NUMBER 107883.SDR CKSA97315Fire Loop · malfunctionedNR 1 ENGINE A FIRE DETECTION LOOP FLUCTUATING (SPIKING INTO RED ZONE). TRANSFERRED TO DMI NR 257 IAW MEL 26-1 CAT C PLACARD INSTALLED. PERFORMED OPERATIONAL CHECK OF NR 1 ENG A LOOP, OPS CHECKS NORMAL ON GROUND. THIS CLEARS DMI 257, PLACARDS REMOVED.SDR CKSA97313Connector · dirtyNUMBER ONE ENGINE FIRE WARNING A-LOOP SHOWS INTERMITTENT FAULT. TRANSFERRED TO DMI NUMBER 250 IN ACCORDANCE WITH MEL 26-1 CATAGORY C PLACARDS INSTALLED. CLEANED FIRE LOOP CONNECTORS ON ENGINE, OPS CHECKS GOOD IAW 26-12-00. THIS CLEARS DMI 250 PLACARDS REMOVSDR CKSA97279Wire · brokenNR 1 ENGINE A FIRE DETECTOR LOOP FLUCTUATING FULL SCALE. TRANSFERRED TO DMI NR 242 IAW MEL 26-2 CAT C, PLACARDS INSTALLED. REPAIRED BROKEN WIRE AT A-SYSTEM LOOP AT CANNON PLUG, OPS CHECK NORMAL IAW B747 26-11-00. THIS CLEARS DMI 242.SDR CKSA97278Fire Loop · shortedNR 1 ENGINE A FIRE DETECTOR LOOP INTERMITTENTLY SPIKES HIGH CAUSING FAULT LIGHT, B-LOOP OK. FOUND FIRE LOOP-A SYSTEM LOOSE AND TOUCHING COWL. RESECURED, OPS CHECKED ON GROUND IAW CHAPTER 26-00. NO DEFECTS NOTED AT THIS TIME.SDR CKSA97252Bulkhead · crackedDURING HARD LANDING INSPECT, FOUND AFT PRESSURE BULKHEAD PIE SECTION AT 11 O'CLOCK POSITION OUTBOARD FASTENER ROW 16TH FROM TOP HOLE EMITS CRACK. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR ON AFT PRESSURE BULKHEAD PIE SECTION AT 11 O'CLOCK POSITION OTHER FASSDR CKSA97251Bulkhead · crackedDURING C-2 CHECK INSPECTION, FOUND PYLON BULKHEAD, NAC STA 222 FORWARD OUTBOARD DOUBLER CRACKED. REPLACED FORWARD OUTBOARD DOUBLER WITH NEW PART IAW SRM 51-10-01 AND 51-30-02. C-CHECK WORK CARD NUMBER 7TK7197. NON-ROUTINE TASK CARD NUMBER 101932.SDR CKSA97250Floorbeam · dentedDURING C-2 CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT STA 760 FLOORBEAM UPPER FLANGE DENTED LBL 50. REMOVED DAMAGED AREA AND REPAIRED FLANGE (7075-T6) IAW SRM 51-40-04 FIGURE 1. C-CHECK WORK CARD NUMBER 7TK7030. NON-ROUTINE TASK CARD NUMBER 101894.SDR CKSA97249Floorbeam · crackedDURING C-2 CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT STA 780 SIDE GUIDE MOUNTING BRACKET BROKEN AND FLOORBEAM WEB CRACKED MARKED J-72. FABRICATED REPLACEMENT MOUNTING BRACKET IAW SRM 53-10-21 AND 51-30-02. REPAIRED CRACKED WEB (7075-T6) IAW SRM 51-40SDR CKSA97248Floorbeam · brokenDURING C-2 CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT STA 580 FLOORBEAM FLANGE BROKEN OFF OUTBOARD OF SEAT TRACK LBL 28 MARKED J-47. REPAIRED BROKEN FLANGE (7075-T6) IAW SRM 51-40-04. C-CHECK WORK CARD NUMBER 7TK7030. NON-ROUTINE TASK CARD NUMBER 101SDR CKSA97247Support · crackedDURING C-2 CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT STA 766 FLOOR PANEL END SUPPORT BENT AND CRACKED LBL 28 MARKED J-55. REMOVED DAMAGED SUPPORT. MANUFACTURED NEW PART (7075-T6) IAW SRM 53-10-21, 51-10-02 MM 51-21-02 AND SRM 51-30-02. C-CHECK INSPESDR CKSA97246Bulkhead · crackedDURING C-2 CHECK INSPECTION, FOUND PYLON BULKHEAD, NAC STA 222 AFT OUTBOARD DOUBLER CRACKED. REPLACED AFT OUTBOARD DOUBLER WITH NEW PART IAW SRM 51-10-01 AND 51-30-02. C-CHECK WORK CARD NUMBER 7TK7197. NON-ROUTINE TASK CARD NUMBER 101933.SDR CKSA97245Shear Tie · crackedDURING C-2 CHECK INSPECTION, FOUND BS 1700 STRINGER 28L SHEAR TIE CRACKED. REPAIRED (2024-T3) IAW BOEING SRM 53-10-04. BOEING MM 5-51-05. NON-ROUTINE TASK CARD NUMBER 101802.SDR CKSA97244Frame · buckledDURING HARD LANDING INSPECTION, FOUND BS 1700 STRINGER 36L FRAME OUTER CHORD BUCKLED. REPAIRED BUCKLED FRAME (2024-T3) IAW B747 SRM 51-40-04. BOEING MM 5-51-05. NON-ROUTINE TASK CARD NUMBER 097900.SDR CKSA97243Shear Tie · crackedDURING HARD LANDING INSPECTION, FOUND BS 1540 FRAME SHEAR TIE CRACKED AT STRINGER 29R. REPAIRED BS 1540 FRAME SHEAR TIE AT STRINGER 29R (2024-T3) IAW B747 SRM 53-10-4 FIGURE 3. BOEING MM 5-51-05. NON-ROUTINE TASK CARD NUMBER 097898.SDR CKSA97242Angle · failedDURING HARD LANDING INSPECTION, FOUND SHEARED HI-LOKS IN 'T' ANGLE AT FS 1500 STRINGER 42R. REMOVED AND REPLACED 'T' ANGLE AT FS 1500 STRINGER 42R IAW (7075-T6) B747 SRM 51-1-0 AND INSTALLED FASTENERS .015625 INCH OVERSIZE IAW B747 SRM 51-30-02, EA 97-136, ANSDR CKSA97241Frame · crackedDURING HARD LANDING INSPECTION, FOUND RIGHT MLG WHEEL WELL STA 1370 CRACK ON OUTBOARD FLANGE OF FRAME APPROXIMATELY 30 INCHES ABOVE WHEEL WELL DOOR MARKED J-30. REPAIRED (2024-T3) IAW BOEING SRM 51-10-02 AND 51-30-03. BOEING MM 5-51-05. NON-ROUTINE TASK CARDSDR CKSA97240Shear Tie · crackedDURING HARD LANDING INSPECTION, FOUND BS 160 STRINGER 26L SHEAR TIE CRACKED AFT LEG ABOVE FLOOR. REPAIRED (2024-T3) IAW BOEING SRM 53-10-04. BOEING MM 5-51-05. NON-ROUTINE TASK CARD NUMBER 101798.SDR CKSA97239Bulkhead · crackedDURING C-2 CHECK INSPECTION, FOUND NAC STA 222 BULKHEAD 'T' EXTRUSION AT NAC WL 181.6 OUTBOARD FORWARD FASTENER HOLE CRACKED FROM HOLE TO EDGE. REPAIRED CRACK AT FORWARD FASTENER HOLE (7075-T6) IAW 54-11-03 FIGURE 8. C-CHECK WORK CARD NUMBER 7TK7198. NON-ROSDR CKSA97238Clip · crackedDURING C-2 CHECK INSPECTION, FOUND FS 260 RIGHT NLG TUNNEL HAS STIFFENER CORNER CLIP (TOP OF NOSE WHEELWELL PRESSURE BULKHEAD 10 INCHES FROM RIGHT SIDE) IS CRACKED MARKED S-14. REMOVED AND REPLACED CLIP (7075-T6) IAW B747 SRM CHAPTER 51-30-02 AS REQUIRED AND SDR CKSA97237Clip · crackedDURING C-2 CHECK INSPECTION, FOUND FS260 LEFT NLG TUNNEL HAS STIFFENER CORNER CLIP (TOP OF NOSE WHEEL WELL PRESSURE BULKHEAD 22 INCHES FROM LEFT SIDE) IS CRACKED MARKED S-13. REMOVED AND REPLACED CLIP (7075-T6) IAW B747 SRM CHAPTER 51-30-02 AS REQUIRED AND 51SDR CKSA97236Clip · crackedDURING C-2 CHECK INSPECTION, FOUND FS260 LEFT NLG TUNNEL HAS STIFFNER CORNER CLIP (TOP OF NOSE WHEEL WELL PRESSURE BULKHEAD 34 INCHES FROM LEFT HAND SIDE) IS CRACKED MARKED S-15. REMOVED AND REPLACED CLIP (7075-T6) IAW B747 SRM CHAPTER 51-10-1 AND 51-30-02 ASSDR CKSA97235Clip · crackedDURING C-2 CHECK INSPECTION, FOUND FS341 LEFT NLG TUNNEL HAS TWO STIFFENER CORNER CLIPS ON SIDE NLG PRESSURE BULKHEAD ARE CRACKED MARKED S-8. REMOVED AND REPLACED CLIPS (7075-T6) IAW B747 SRM CHAPTER 51-30-02 AS REQUIRED AND 51-10-1. C-CHECK WORK CARD NUMBERSDR CKSA97234Clip · crackedDURING C-2 CHECK INSPECTION, FOUND FS 340 LEFT NLG TUNNEL HAS STIFFENER CORNER CLIP ON SIDE NLG PRESSURE BULKHEAD IS CRACKED MARKED S-7. REMOVED AND REPLACED CLIP (7075-T6) IAW B747 SRM 51-30-02 AND 51-10-1. C-CHECK WORK CARD NUMBER 7TK9031. NON-ROUTINE TASSDR CKSA97233Skin · wrinkledDURING HARD LANDING INSPECTION, FOUND LEFT FUSELAGE SKIN WRINKLED, SKIN PANEL NR 16 STA 1480 TO STA 1740 STRINGER 23 TO STRINGER 34. INSTALLED NEW SKIN FROM STA 1480 - STA 1741 STRINGER 23L - STRINGER 34L IAW B747 DRAWING 65B04131-5002 REV J. ALL REMOVED HI-LSDR CKSA97232Shear Tie · deformedDURING HARD LANDING INSPECTION, FOUND TWO SHEAR TIES ARE SLIGHTLY DEFORMED ON THE FLANGE COMMON TO THE SKIN BETWEEN STRINGER 38R AND STRINGER 40R FS 1540. REMOVED AND REPLACED 2 EACH SHEAR TIES (2024-T3) IAW B747 SRM 51-10-1 AND 51-30-02, EA 97-136. BOEING MSDR CKSA97231Floorbeam · damagedDURING C-2 CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT STA 570 HOLE IN FLOORBEAM RADIUS AT CORNER OF BALLMAT LBL 23 MARKED J-46. REMOVED DAMAGED AREA AND REPAIRED (7075-T6) IAW SRM 51-40-03 FIGURE 1. C-CHECK WORK CARD NUMBER 7TK0125. NON-ROUTINE TASK SDR CKSA97230Skin · gougedDURING CPCP CHECK INSPECTION, FOUND FORWARD LOWER CARGO DOOR IS GOUGED AND DENTED IN AT LOWER CORNER MARKED J-44. REPAIRED DAMAGED AREA ON FORWARD LOWER CORNER (2024-T3) IAW SRM 52-00-03 FIGURE 4. CPCP TASK CARD NUMBER C52-735-03. NON-ROUTINE TASK CARD NUMBSDR CKSA97229Skin · crackedDURING C-2 CHECK INSPECTION, FOUND CRACKED SKIN DOUBLER ON MID FLAP OUTBOARD TRAILING EDGE END OF INBOARD FLAPS. REPAIRED CRACK (2024-T3) IAW B747 SRM 51-40-03. C-CHECK WORK CARD NUMBER 7TK7171. NON-ROUTINE TASK CARD NUMBER 101747.SDR CKSA97228Skin · delaminatedDURING C-2 CHECK INSPECTION, FOUND RIGHT WING OUTBOARD MIDFLAP HAS DELAMINATION ON LEADING EDGE NEAR NUMBER 4 ENGINE PYLON. REPAIRED DELAMINATED RIGHT WING OUTBOARD MIDFLAP ON LEADING EDGE NEAR NUMBER 4 ENGINE PYLON IAW BOEING SRM 51-40-12. C-CHECK WORK CARDSDR CKSA97227Bulkhead Web · crackedDURING C-2 CHECK INSPECTION, FOUND NAC STA 222 AFT OUTBOARD BULKHEAD WEB CRACKED. REMOVED AND REPLACED CRACKED BULKHEAD WEB WITH NEW PART IAW SRM 51-10-01 AND 51-30-02. C-CHECK WORK CARD NUMBER 7TK7194. NON-ROUTINE TASK CARD NUMBER 102133.SDR CKSA97226Bulkhead Web · crackedDURING C-2 CHECK INSPECTION, FOUND NAC STA 222 OUTBOARD FORWARD BULKHEAD WEB CRACKED. REMOVED AND REPLACED CRACKED BULKHEAD WEB WITH NEW PART IAW SRM 51-10-01 AND 51-30-02. C-CHECK WORK CARD NUMBER 7TK7194. NON-ROUTINE TASK CARD NUMBER 102143.SDR CKSA97225Skin · wrinkledDURING HARD LANDING INSPECT, FOUND SKIN PNL AT STA 1961 - STA 2161 STR 34R - STR 46R HAS WRINKLES OVER THE ENTIRE SKIN (MEASURING .020 - .030 IN DEPTH) (FS 1961 - FS 1980 STR 42R - STR 46R MEASURE .10 IN DEPTH). INSTALLED ALUMINUM SHIMS BETWEEN THE EXISTING SSDR CKSA97224Bulkhead Web · buckledDURING HARD LANDING INSPECTION, FOUND AFT PRESSURE BULKHEAD PIE SECTION SKIN AT 11 O'CLOCK POSITION BUCKLED. REMOVED AND REPLACED WEB GORE PER BOEING ENGINEERING RECOMMENDATIONS AND MSG CKF-ORD-97-0017RE PROCEDURES, EA 97-136, AND BOEING 8110-3 DATED 18 MAY 9SDR CKSA97223Web · bulgedDURING HARD LANDING INSPECTION, FOUND SEVERAL BULGES ON KEEL BEAM WEB IN LEFT WING MLG WELL. PER BOEING RECOMMENDATION LEFT WEB (PANEL) WAS REMOVED AND REPLACED (2024-T3) PER BOEING MSG CKF-ORD-97-0024RE DATED 17 APR 97 AND BOEING DRAWING 65B15069-345 PERFORMSDR CKSA97222Web · bulgedDURING HARD LANDING INSPECTION, FOUND SEVERAL BULGES ON KEEL BEAM WEB IN LEFT BODY MLG WELL. PER BOEING RECOMMENDATION LEFT WEB (PANEL) WAS REMOVED AND REPLACED (2024-T3) PER BOEING MSG CKF-ORD-97-0024RE DATED 17 APR 97 AND BOEING DRAWING 65B15069-345. PERFOSDR CKSA97221Web · bulgedDURING HARD LANDING INSPECT, FOUND SEVERAL BULGES ON KEEL BEAM WEB IN RIGHT WING MLG WELL. PER BOEING RECOMMENDATION RIGHT WEB WAS REMOVED AND REPLACED (2024-T3) PER BOEING MSG CKF-ORD-97-0024RE DATED 17 APR 97 AND BOEING DRAWING 65B15069-346 PERFORMED HFEC ISDR CKSA97220Web · bulgedDURING HARD LANDING INSPECTION, FOUND SEVERAL BULGES ON KEEL BEAM WEB IN RIGHT BODY MLG WELL. PER BOEING RECOMMENDATION RIGHT WEB (PANEL) WAS REMOVED AND REPLACED (2024-T3) PER BOEING MSG CKF-ORD-97-0024RE DATED 17 APR 97 AND BOEING DRAWING 65B15069-346, PERFSDR CKSA97219Web · deformedDURING HARD LANDING INSPECTION, FOUND THE HORIZONTAL WEB AT WL 116 (UPPER WEB) SHOWS DEFORMATION LEFT SIDE AN .040 BULGE FROM STA 1340 TO STA 1350 AND .050 THRU .080 WARPS FROM STA 1270 TO STA 1340 RIGHT SIDE AN .060 BULGE AT STA 1340 THRU STA 1350 AND .010 WASDR CKSA97218Web · buckledDURING HARD LANDING INSPECTION, FOUND HORIZONTAL WEB SHOWS SIGNS OF BUCKLING AT STA 1265 TO STA 1346. PER BOEING RECOMMENTDATION HORIZONTAL WEB PANEL WAS REMOVED AND REPLACED (2024-T3) PER BOEING MSG M-7240-97-0629 PERFORMED HFEC INSPECT TO ALL HOLES AND INSSDR CKSA97217Web · bulgedDURING HARD LANDING INSPECTION, FOUND SEVERAL BULGES ON WEB ABOVE KEEL BEAM LEFT WING MLG WELL AREA. KEEL BEAM CENTER WEB FROM STA 1265 THRU STA 1350 WAS REMOVED AND REPLACED PER BOEING MSG CKF-ORD-97-0024RE DATED 17 APR 97. BOEING MM 5-51-05. NON-ROUTINE TSDR CKSA97216Web · corrodedDURING HARD LANDING INSPECTION, FOUND SEVERAL BULGES ON WEB ABOVE KEEL BEAM RIGHT WING MLG WELL AREA. KEEL BEAM WEB FROM STA 1265 THRU STA 1350 WAS REMOVED AND REPLACED PER BOEING MSG CKF-ORD-97-0024RE DATED 17 APR 97. BOEING MM 5-51-05. NON-ROUTINE TASK CASDR CKSA97215Bulkhead Web · bulgedDURING HARD LANDING INSPECTION, FOUND SEVERAL BULGES ON FS1480 BULKHEAD IN LEFT BODY MLG WELL. OK TO INSTALL REPAIR DOUBLER IAW BOEING DRAWING 65B15085 DATED 26 APR 97, BOEING ENGINEER RECOMMENDS REPAIR TO THE BUCKLE AREA LOCATED AT THE LEFT SIDE PER BOEING MSDR CKSA97214Bulkhead Web · bulgedDURING HARD LANDING INSPECTION, FOUND SEVERAL BULGES ON FS1480 BULKHEAD IN RIGHT BODY MLG WELL. BOEING ENGINEER RECOMMENDS REPAIR TO THE BUCKLE AREA LOCATED AT RIGHT SIDE PER BOEING MSG CKS-ORD-97-0037RE, CKF-ORD-97-0039RE AND BOEING DRAWING 65B28016-14. BOESDR CKSA97213Skin · wrinkledDURING HARD LANDING INSPECTION, FOUND RIGHT FUSELAGE SKIN PANEL MARKED NR 1A FROM STA 1480 TO STA 1740 STR 23 TO STR 34 HAS SEVERAL AREAS OF WRINKLED SKIN. INSTALLED NEW SKIN FROM STA 1480 THRU STA 1741 STRINGER 23R THRU STRINGER 34R IAW B747 DRAWING 65B04131SDR CKSA97212Skin · wrinkledDURING HARD LANDING INSPECTION, FOUND RIGHT FUSELAGE SKIN MARKED NR 2C AT STA 1740 STRINGER 40 TO STRINGER 46 HAS WRINKLED SKIN. CHECK LIMITS. DAMAGED SKIN CITED ABOVE WERE CUT, REMOVED AND PERFORMED COMBINED REPAIRS (2024-T3) IAW B747 SRM 53-30-03 FIGURE 48SDR CKSA97211Skin · wrinkledDURING HARD LANDING INSPECT, FOUND RT FUSELAGE SKIN MARKED NR 2D AT STA 1740 AT STRINGER 46 HAS WRINKLED SKIN. REPAIRED SKIN (2024-T3) IAW B747 SRM 53-30-03 FIGURE 48. BOEING MM 5-51-05. NON-ROUTINE TASK CARD NUMBER 098051.
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