Boeing 737-83N
Service difficulty reports · 1,087
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 = '73783N' 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 = '73783N' 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 SCNA20250910373Window · arcedARCING ON UPPER INBOARD SIDE OF R1 WINDSCREEN. R&R R1 WINDOW PER AMM 56-11-11. LEAK CHECK AND OPS CHECKS GOOD REMOVED COLLARS AND REST BREAKERS ON P18-3,B1,B3,D1,D2,E1,E2 P6-3 A9,A10 P6-11B,B8,B9 P6-12 B8,B9SDR SCNA20250904355Bulb · inoperativeINOPERATIVE BULB ON THE EMER EXIT LIGHT NOT ARMED LIGHT. RELAMPED OPS CHECK GOOD IAW AMM 33-11-00SDR SCNA20250902344Comms Unit · faultedCAPT COMMS HAVE LOUD FEEDBACK ISSUE IN ALL MODES INCLUDING RADIO TRANSMIT AND ICG. AUDIO WARNINGS ARE EXTERMELY LOUD AND NOT SAFE FOR FLIGHT. PERFORMED OPS TEST ON ACP IAW AMM TASK 23-51-02-400-801 & FOUND OBS ACP WAS CAUSING STATIC FEEDBACK ON CAPT SPEAKER SDR SCNA20250829343Nut Plate · missingREMOVED ESCAPE SLIDE GIRT BAR BRACKETS FOM, AFT ADAPTER PLATE AFT SCREW NUTPLATE FOUND TO BE MISSING, RTV HELD SCREW IN PLACE. REMOVE ESCAPE SLIDE GIRT BAR BRACKETS FOM, REF AMM 25-66-02. INSTALLED NUT PLATE AMM20-20 INSTALLED L1 DOOR ESCAPE SLIDE GIRT BAR SDR SCNA20250827338Insert · looseL1 DOOR ENTRY GALLEY MAT THRESHOLD PLATE HAS LOOSE INSERTS IN FLOORBOARD BETWEEN GIRT BAR FLOOR MOUNTS. INSTALLED NEW INSERTS AND SECURED THRESHOLD PLATE.SDR SCNA20250820328Battery Pack · no testEMERGENCY LIGHTING BATTERY PACK AT POSITION M1670 FAILED CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK AT POSITION M1670 REF. AMM 33-51-06, OPS CHECK GOOD.SDR SCNA20250820327Battery Pack · no testEMERGENCY LIGHT BATTERY PACK AT POSITION M1675 FAILED CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK AT POSITION M1675 REF. AMM 33-51-06, OPS CHECK GOOD.SDR SCNA20250818323Filter · odorDEFECT 802437: VERY PUNDJENT MUSTY SMELL COMING THROUGH THE AIR VENTS ON DECENT AND ONLY ON DESENT RESOLUTION: REMOVED AND REPLACED LEFT & RIGHT RECIRCULATION HEPA FILTERS. REF. 21-25-01-400-801. REMOVED AND REPLACED EQIP COOLING FAN FILTER REF 27-21-01-400-80SDR SCNA20250807300Outflow Valve · fluctuatesDURING DESCENT, OUTFLOW VALVE FLUCTUATED TOWARDS OPEN AT LARGE INTERVALS ON 3 SEPARATE OCCASIONS (23,000' 16,500' & 10,000'). THIS RESULTED IN CABIN CLIMB RATES OF 3000 FPM AND PRESSURE DIFFERENTIALS THAT COULD BE FELT IN THE PILOTS EARDRUMS. NO CAUTION LIGHTSSDR SCNA20250731292Oven · dirtyAFT OVENS NEED CLEANING.CREATE SMOKE WHEN USED SET OFF FIRE ALARM. REPLACED AFT OVENS INSERTS REF AMM 25-31-02SDR SCNA20250731289Switch · crew errorFORWARD LAV. EMERGENCY LIGHT INOP. THE NO SMOKE/FASTEN SEAT BELT LIGHT SWITCH WAS IN THE OFF POS. FWD LAV. PER AMM 33-25-00SDR SCNA20250728276Power Supply · faultedWHILE PERFORMING EMERGENCY LIGHT TEST FOUND THE FWD LH AREA EMER LIGHTS INOP. REPLACED THE FWD AREA EMERGENCY LIGHT POWER SUPPLY ASSY IAW AMM 33-51-06 AND OPS CHECK GOODSDR SCNA20250721266Bracket · looseDEFECT 801438: 1 R DOOR SLIDE BRACKETS LOOSE. REMOVED 1 R DOOR SLIDE PACK. INSTALLED NEW RIVET IN RIGHT GRIT BAR RETAINER CLIP.IAW SRM 51-40-02.INSTALLED SLIDE PACK IAW AMM 25-66-01 OK FOR SERVICESDR SCNA20250716262Nut · undertorquedDURING CLIMB OUT, OIL QUANTITY IN #2 ENGINE DECREASED TO ZERO, DID NOT MOVE FROM ZERO FOR REST OF FLIGHT, ALL OTHER INDICATIONS REMAINED NORMAL. RETORQUED ENGINE OILTANK OIL IN COUPLING NUT IAW AMM 79-11-01, PERFORMED IDLE LEAK CHECK 3A AND PART POWER LEAK CHESDR SCNA20250714257Engine · failedSEVERE ENGINE DAMAGE #2 CLIMBING OUT OF 14,000 FT REDLINE EGT NO ROTATION N2 N1 14% FA'S REPORTED ALOT OF SPARKS MODERATE VIBRATION. REMOVED AND REPLACED #2 ENGINE REF TASK CARD # 710000000 ACCOMPLISHED ENGINE RUN TEST 9 AND TEST 5 REF AMM 71-00-00 ALL SYSTESDR SCNA20250714256Battery Pack · inoperativeLEFT AND FWD GALLEY EMERGENCY LIGHTS INOP. R&R L1 EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06, OPS CHECK OKAY.SDR SCNA20250714258Sensor · faultedDEFECT 801870: TRAILING EDGE FLAP ASYMMETRY RT FLAP INDICATOR SHOWS UP, LEFT FLAP INDICATOR SHOWS LESS THAN UP. - (EMERGENCY DECLARED) - RESOLUTION: FSEU BITE PROCEDURE INDICATED FLAP SKEW FAULT 27-53409. NO 28VAC WAS PRESENT AT PIN 2 OF #4 SKEW SENSOR . FOSDR UIEA2025071100906Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 138.7, 23" FROM FRONT SPAR.(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT LOWER SKIN R/H HORIZONTAL STABILIZER STA 138.7, 23" FROM FRONT SPAR IAW B737 SRM 55-10-01-2R-1SDR UIEA2025071100907Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 101 FROM FRONT SPAR.(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT LOWER SKIN R/H HORIZONTAL STABILIZER STA 101 FROM FRONT SPAR IAW B737 SRM 55-10-01-2R-11, REPAIR 11 FSDR UIEA2025071100908Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 147.9, 14.72" FROM FRONT SPAR.(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 147.9, 14.72" FROM FRONT SPAR, MATERIAL USED: DOUBSDR UIEA2025071100909Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 138.7, 9.02" FROM AFT SPAR.(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT LOWER SKIN R/H HORIZONTAL STABILIZER STA 138.7, 9.02" FROM AFT SPAR IAW B737 SRM 55-10-01-2R-1SDR UIEA2025071100910Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 175.5, 10" FROM T/E BEAM. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT LOWER SKIN R/H HORIZONTAL STABILIZER STA 175.5, 10" FROM T/E BEAM IAW B737 SRM 55-10-01-2R-11, REPSDR UIEA2025071100914Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 147.9, 7.09" FROM FRONT SPAR. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 147.9, 7.09" FROM FRONT SPAR, MATERIAL USED: DOUBLER SDR UIEA2025071100915Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 138.7, 9" FROM AFT SPAR. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 138.7, 9" FROM AFT SPAR, MATERIAL USED: DOUBLER REPAIR (20SDR UIEA2025071100916Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 101.9, 9.05" FROM AFT SPAR. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 101.9, 9.05" FROM AFT SPAR, MATERIAL USED: DOUBLER REPASDR UIEA2025071100917Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 101.9, 18.83" FROM AFT SPAR. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 101.9, 18.83" FROM AFT SPAR, MATERIAL USED: DOUBLER RESDR UIEA2025071100918Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN, A CRACK NOTED ON STAB HORIZ AT STA 138.7, 16.96" FROM AFT SPAR. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AT L/H HORIZONTAL STABILIZER LOWER SKIN STA 138.7, 16.96" FROM AFT SPAR, MATERIAL USED: DOUBLER RESDR UIEA2025071100919Stiffener · crackedR/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #4 CRACKED LOWER SIDE.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON R/H HORIZONTAL STABILIZER RIB #2 STA 92.7 STIFFENER #4 LOWER SIDE 37.3" FROM FRONT SPAR, MEASURED CRACK 0.562" ISDR UIEA2025071100920Stiffener · crackedR/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON R/H HORIZONTAL STABILIZER RIB #2 STA 92.7 STIFFENER #3 LOWER SIDE 28" FROM FRONT SPAR, MEASURED CRACK 1.687" IAWSDR UIEA2025071100921Stiffener · crackedR/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #2 CRACKED LOWER SIDE.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON R/H HORIZONTAL STABILIZER RIB #2 STA 92.7 STIFFENER #2, MEASURED CRACK 1.812" IAW B-737 SRM 55-10-09-2R-4 REPAIRSDR UIEA2025071100922Stiffener · crackedR/H HORIZONTAL STABILIZER NUMBER 6 STA 129.5 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(<P>ACCOMPLISHED AT R/H HORIZONTAL STABILIZER RIB #6 STA 129.5 STIFFENER #3, <SPAN>CATEGORY "A" REPAIR, PERMANENT REPAIR. LOCATION 23" FROM FRONT SPAR,</SPAN><SPAN> CRACSDR UIEA2025071100923Stiffener · crackedR/H HORIZONTAL STABILIZER NUMBER 10 STA 166.3 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON R/H HORIZONTAL STABILIZER RIB #10 STA 166.3 STIFFENER #3 AT 21" FROM FRONT SPAR, MEASURED CRACK 1.750" IAW B-7SDR UIEA2025071100924Stiffener · crackedL/H HORIZONTAL STABILIZER NUMBER 2 STA 92.7 HAS VERTICAL STIFFENERS #3 CRACKED LOWER SIDE.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON L/H HORIZONTAL STABILIZER RIB #2 STA 92.7 STIFFENER #3, MEASURED CRACK 2.100", LOCATED 28" FROM FRONT SPAR APROXSDR SCNA20250711253Battery Pack · inoperativeROW 15-22 EMERGANCY LIGHTS OUT.R & R EMERGANCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECKS GOOD.SDR SCNA20250625231Slide · not reportedR1 DOOR SLIDE UNUSABLE . R&R R1 SIDE IAW AMM 25-66-01 OK FOR SERVICE.SDR UIEA2025061200741Skin · scratchedLOWER LOBE, FWD CARGO DOOR EXTERNAL SKIN WITH SCRATCHES LOCATED BETWEEN BEAM D AND LOWER FRAME.(<P>REPLACED FWD CARGO COMPARTMENT DOOR EXTERNAL SKIN I.A.W B737-800 BCF SRM 52-30-01-2R-3 REPAIR 3 PARAGRAPH 4 TABLE 201 FIGURE 202 REV 23 AND BOEING REF DWG NO: 14SDR UIEA2025061200743Skin · scratchedLOWER LOBE, AFT CARGO COMPARTMENT DOOR, EXTERNAL SKIN WITH SEVERAL SCRATCHES BETWEEN BEAM B AND LOWER FRAME.(<P>REPLACED AFT CARGO COMPARTMENT DOOR EXTERNAL SKIN IAW BOEING 737-800 BCF SRM 52-30-01-2R-3 REPAIR 3 PARAG 4 TABLE 201 FIG 203 REV 23 AND BOEING REF SDR UIEA2025061200744Cargo Track · crackedFWD CARGO COMPARTMENT, CARGO TRACK-TIE DOWN AT STA 460 RBL 13.84 WITH CRACK.(<P>REPAIRED TIE DOWN CARGO TRACK AT FWD CARGO COMPARTMENT RBL 13.84", SECTION BETWEEN B/S 400 AND B/S 500 +17.75", SPLICED BETWEEN B/S 500 AND B/S 500A I.A.W B737-800 BCF SRM 53-00-53SDR UIEA2025061200746Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE AT STA 727+13" RBL3 RAIL CHANNEL WITH CORROSION.(<P>REPAIRED RAIL FLOOR BEAM SECTION AT AFT CARGO COMPARTMENT FLOOR STRUCTURE RBL 3" FROM B/S 727 +8" TO B/S 727B +14", SPLICED BETWEEN B/S 727B AND B/S 727C I.A.W B737-800 BSDR UIEA2025061200747Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE FROM STA 747 TO STA 847 AT LBL 21" SIDE PLATE-SUPPORT ZEE WITH CORROSION IN SEVERAL PLACES.(<P>REPAIRED AFT CARGO COMPARTMENT ZEE CHANNEL SIDE PLATA SECTION AT LBL 21" FROM B/S 727J +3.5" TO B/S 847, SPLICED BETWEEN B/S 72SDR UIEA2025061200748Support Angle · crackedUPPER FUSELAGE AT STA 303.9 LBL 57 WL 208.1, FWD ENTRY AREA SILL SUPPORT ANGLE WITH CRACK.(<P>REPAIRED FWD ENTRY DOOR LOWER SILL INNER CHORD SECTION AT B/S 303.9 WL 208 LBL 57 IAW COO-EO-2025-22233-R00 REV 00. APPROVED BY FAA DER ROBERT MANASHI (DER NUMBER 876SDR UIEA2025061200749Frame · unknownPER CUSTOMER INSTRUCTIONS IN REFERENCE AT BOEING RECOMENDATION REPLACE RH FRAME FITTING AND FAIL SAFE STRAP ASSY AT STATION 663.75 PER ENGINEERING DRAWING 144A2400-28 FRAME INSTALLATION.(<P>PERFORMED RH STA 663.75 FRAME FITTING AND SAFE STRAP REPLACEMENT AND BSDR UIEA2025061200750Failsafe · damagedIN REFERECE AT COOPESA´S NRI 1-23 REPLACE LH FRAME FITTING AND FAIL SAFE STRAP ASSY AT STATION 663.75 PER ENGINEERING DRAWING 144A2400-27 FRAME INSTALLATION.(<P>PERFORMED LH STA 663.75 FRAME FITTING AND SAFE STRAP REPLACEMENT AND BLEND OUT REPAIR (CATEGORY A SDR UIEA2025061200751Stringer · nonePERFORM CUTTING AND SPLICING OF STRINGER 10 L/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0061 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 14.(<P>PERFORMED SPLICE REPAIR OF FUSELAGE STRINGER 10LH BTWN STA 663.75 ASDR UIEA2025061200752Stringer · nonePERFORM CUTTING AND SPLICING OF STRINGER 14 L/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0062 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 24.(<P><SPAN LANG="EN-US">PERFORMED SPLICE REPAIR OF FUSELAGE STGR 14L BTWSDR UIEA2025061200753Stringer · nonePERFORM CUTTING AND SPLICING OF STRINGER 10 R/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0063 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 14.<BR>(<P>PERFORMED SPLICE REPAIR OF FUSELAGE STINGER 10 RH, BETWEEN STA SDR UIEA2025061200754Stringer · nonePERFORM CUTTING AND SPLICING OF STRINGER 14 R/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0064 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 24. PERFORMED SPLICE REPAIR OF FUSELAGE STGR 14R BETWEEN B/S 663.75 AND BSDR UIEA2025061200755Skin · dentedENGINE #2, INLET COWL, INNER BARREL, LOWER ACUSTICAL SKIN WITH DENTS (2 EA) AT 6 O'CLOCK POSITION. PERFORMED PERMANENT REPAIR AT ENGINE N°2 INLET COWL INNER BARREL I.A.W ATLAS AIR ENGINEERING AUTHORIZATION EA-1971A215 REV 0 DATED 27-MAY-25. NO FURTHER DEFECTSDR UIEA2025061200756Skin · crackedLEFT WING, INBOARD L/E (FIXED L/E) SKIN CRACKED AT KRAS 217.5 AROUND FASTENER HOLE (1EA) AND AT SEAL RIB (REF: KRAS 224.82) BETWEEN THE NOSE BEAM AND FIRST STRINGER (2EA).(<P>PERFORMED LH WING AT REF KRAS 224.82 AND REF KRAS 217.5 FIXED LEADING EDGE SKIN PANELSDR UIEA2025061200757Support Beam · wornLOWER FUSELAGE, LOWER SUPPORT BEAM AT RBL 40.875, STA 547 LOWER CHORD WITH WEAR. REPAIRED WING CENTER SECTION LOWER SUPPORT BEAM LOWER CHORD SECTION AT RBL 40.875 B/S 547 IAW SRM 57-10-13-2R-3 REPAIR 3 FIG 202 DETAIL C, REV 23 DATED 10-MAR-25. THIS IS A CATEG
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