Boeing 737-76N
Service difficulty reports · 4,807
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 = '73776N' 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 = '73776N' 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 SWAA2025021983951Shield · corroded(A204 DOT 78) FWD CARGO STA 492; RBL 21; WL 155; SPLASH SHIELD HAS CORROSION ON UPPER SURFACE<[01] REMOVED CORROSION AND VERIFIED WITH A 10-POWER MAGNIFYING GLASS ON FWD CARGO STA 492; RBL 21; WL 155; SPLASH SHIELD UPPER SURFACE I.A.W SRM 51-10-02-0G-0 VERIFIESDR SWAA2025021984185Floor Panel · corrodedFWD CARGO FLOOR PANEL 120CF HAS CORROSION AT FASTENER HOLES<[01] UPON FURTHER INVESTIGATION FOUND THAT CORROSION WAS 30 INCHES IN LENGTH WITH A MAX ALLOWED LENGTH OF 3 INCHES FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1; RECEIVED REPLACEMENT MATERIAL PN 202SDR SWAA2025022083595Rib · cracked(A204 DOT 64) LH HORIZONTAL STAB LEADING EDGE 331B; LE STA 114.5; RIB IS CRACKED NEXT TO BEND RADIUS AT LOWER AFT HOLE.<[01] REMOVED L/H L/E HORZ STAB RIB AT STA114.5 IAW SRM 51-40-02-0G-0 AND DWG 186A1305 REV - VERIFIED PART USING P/N 186A1352-9 AND ATAG WN49SDR SWAA2025022083596Rib · buckledLH HORIZONTAL STAB LEADING EDGE 331B; LE STA 198.25; RIB IS BUCKLED AT AFT RADIUS.<[01] REMOVED L/H HORZ STAB L/E 331B RIB IAW SRM 51-40-02-0G-0 AND DWG 186A1001 REV A VERIFIED PART USING P/N 654A0004-685 ATAG A285988 AND DWG 186A1001 REV A INSTALLED RIB IAW SSDR SWAA2025022083779Angle · corrodedDOT#10 A-043 AFT CARGO COMPARTMENT LH Z ANGLE CORRODED STA 727E+6' TO 727D+3' LBL 24 WL 156<[01] REMOVED CORRSION IAW SRM 51-10-02-0G-0<BR>UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .032'; LOSS .013'; REMAINING .019'. TOOL#40084; DUE 06AUG25<BR>EVALUATED ARSDR SWAA2025022083780Angle · corrodedDOT#11 A-043 AFT CARGO COMPARTMENT LH Z ANGLE CORRODED STA 727E+14' TO 787+5' LBL 24 WL 156<[01] REMOVED CORRSION IAW SRM 51-10-02-0G-0<BR>UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .032'; LOSS .010'; REMAINING .022'. TOOL#40084; DUE 06AUG25<BR>EVALUATED ARSDR SWAA2025022083781Shield · corrodedDOT#13 A-043 AFT CARGO COMPARTMENT RH FWD SHIELD CORRODED STA 767 TO 787 RBL 24 WL 156<[01] REMOVED CORRSION ON TOP SIDE OF SHIELD IAW SRM 51-10-02-0G-0 EVALUATED AREA. ORGININAL THICKNESS 0.050'. LOSS 0.010'. REMAINING THICKNESS 0.040'. MAX. OF 10T ON ALLOWABSDR SWAA2025022083782Angle · corrodedDOT#14 A-043 AFT CARGO COMPARTMENT RH Z ANGLE CORRODED STA 727+4 TO 767 RBL 24 WL 156<[01] REMOVED CORRSION IAW SRM 51-10-02-0G-0; UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .032'; LOSS .009'; REMAINING .023'. TOOL#40084; DUE 06AUG25; EVALUATED AREA. ORGINISDR SWAA2025022083772Web · corrodedDOT#03 A-043 AFT CARGO COMPARTMENT DOOR SILL WEB CORRODED STA 807+3' TO 827+4' RBL 27 WL 156<[01] VERIFIED ALL NDT TASK COMPLETE;[02] 01 - REMOVED AND REPLACED AFT CARGO PIT LOWER DOOR SILL WEB PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION ANDSDR SWAA2025022083776Web · corrodedFWD CARGO DOOR CUTOUT LOWER SILL WEB HAS EVIDENCE OF CORRION IN SEVERAL AREAS OF WEB<[01] 01 - REMOVED AND REPLACED PER SRM 53-30-15-1A-1-A00071.SDR SWAA2025021983778Strap · corrodedDOT#08 A-043 AFT CARGO COMPARTMENT FLOORBOARD 'T' STRAP CORRODED STA 727D RBL 2 WL 156<[01] REPLACED AFT CARGO COMPARTMENT FLOORBOARD 'T' STRAP P/N 146A9401-8 TAG#49635 IAW IPC 53-42-11-30 INSTALLED ON W/O TTG8Q00WXN8W;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2025021983777Angle · corrodedDOT#07 A-043 AFT CARGO COMPARTMENT RH 'Z' ANGLE CORRODED STA 887+8 RBL 24 WL 156<[01] EVALUATED AREA. ORGININAL THICKNESS 0.032'. LOSS 0.012'. REMAINING THICKNESS 0.020'. MAX. OF 10T ON ALLOWABLE DAMAGE. OUT OF LIMITS IAW SRM 53-00-53-1A-2<BR>FABRICATED NEW Z SDR SWAA2025021983773Attach Angle · corrodedDOT#05 A-043 AFT CARGO COMPARTMENT FWD BKHD LOWER CENTER FAIRING ATTACH ANGLE TOP STRAP CORRODED STA 727+4' RBL 20 WL 156<[01] REPLACED (PLATE) AFT CARGO COMPARTMENT P/N453A2611-12 TAG#A289211 IAW IPC 25-52-10-02 INSTALLED ON W/O TTG8Q00WXN8W;[02] REPLACED (PLSDR SWAA2025021983594Hook · corroded(A204 DOT 59) RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAS MINOR CORROSION<[01] 01 - REMOVED AND REPLACED R/H EMERGENCY EXIT DOOR LIFE LINE PER [AMM 25-61-10-400-802-NG (EMERGENCY EXIT DOOR LIFE LINE INSTALLATION - PERMANENT)]<BR><BR>STRAP P/N: 416A1531-17SDR SWAA2025021983593Hook · corroded(A204 DOT 60) LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAS MINOR CORROSION<[01] LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK WAS REMOVED AND REPLACED I.A.W. AMM 25-61-10-400-802-NG<BR><BR>TOOL USED: STAAR 39119; DUE 03/03/25;[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2025021983001Light · crackedEMERGENCY EXIT LIGHT ON FWD LAVATORY IS CRACKED<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON FWD LAVATORY IAW AMM 33-51-01-960-802 STEP 3A-3C(1-4)(5)(D) (6)(7)(10)(12).<BR>SIGNING FOR JOSEPH KREBS EMP#38394;[02] REMOVED AND REPLACED EMERGENCY EXIT LIGHT OSDR SWAA2025022082601Floorboard · pulled154-05 PASSENGER CABIN FLOOR BOARD 231XF HAS MULTIPLE AREAS OF PULLED FIBERGLASS FROM TAPE REMOVAL. REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.SDR SWAA2025021982605Floorboard · pulled154-15 PASSENGER CABIN FLOOR BOARD 242DF HAS MULTIPLE DENTS AND PULLED FIBERGLASS ON SURFACE<[01] 'REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025021982604Floorboard · pulled154-10 PASSENGER CABIN FLOOR BOARD 232SF HAS MULTIPLE DENTS AND PULLED FIBERGLASS ON UPPER SURFACE<[01] 'REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025021982602Floorboard · pulled154-06 PASSENGER CABIN FLOOR BOARD 241AF HAS MULTIPLE AREAS OF PULLED FIBERGLASS ON SURFACE<[01] 'REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025021982851Scuff Plate · crackedFWD CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED<[01] CRACK ON FWD CARGO DOOR FWD CORNER SCUFF PLATE WAS REPIARED ON BACK SHOP WORK ORDER 46301/1400/0001 SERIAL NO: 9519433 IAW SRM 53-30-15-2R-1 (WELD REPAIR);[02] VERIFIED ITEM 1<BR><BR>AUDIT C/WSDR SWAA2025010682617Seat · out of adjustPASSENGER CABIN SEAT RECLINES AT SEAT 11B EMERGENCY EXIT ROW<[01] ADJUSTED RECLINE AT 11B PER CMM 25-23-46.SDR SWAA2025010682626Seat · out of adjustSEAT 11B RECLINING AT EMERGENCY EXIT<[01] READJUSTED SEAT 11B RECLINE LOCK RING AT EMERGENCY EXIT PER CMM 25-21-42SDR SWAA2025022082595Wedge · crackedR/H WING # 5 SLAT LOWER CENTER WEDGE HAS CRACK ON EDGE OF WEDGE. REMOVED R/H WING # 5 SLAT LOWER CENTER WEDGE IAW SRM 51-40-02-0G-0. UT IAW B737 NDT PART 4; 51-00-01. NO ADDITIONAL DEFECTS NOTED. TOOL#31896; DUE 29APR25. EVALUATED AND FOUND SMALL CRACK AT CESDR SWAA2025022082455Attach Fitting · crackedR/H WING TO BODY FAIRING PANEL 191AR AFT EDGE; CENTER ATTACH BEAM IS CRACKED AT UPPER END.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2025022081912Beam · corroded(A-204 DOT 29) LH WING FIXED LEADING EDGE CAVITY. FORWARD EDGE OF KRUEGER FLAP CUTOUT. NOSE BEAM HAS CORROSION IN RADIUS FROM #1 KRUEGER FLAP 2ND FROM I/B HINGE TO #2 KRUEGER FLAP 2ND FROM I/B HINGE<[01] REMOVED DAMAGE AND REPAIRED PER EA 25-157-00351;[02] COMSDR SWAA2025022081640Plate · corroded(A204 DOT 3) #1 FLAP TRACK FORWARD FAIRING. INNTER FORWARD MOUNT PLATE HAS EVIDENCE OF CORROSION<[01] 04 - REPAIRED PER [SRM 57-53-71-1A-1-A00978 (PERMANENT (NON-DENT DAMAGE TYPES))];[02] COMPLETE<BR>AUDIT C/WSDR SWAA2024122680673Lamp · inoperativeL1 DOOR AND R/H MID EMERGENCY EXIT SIGN SEVERAL LAMPS INOP<[01] R&R SEVERAL LAMPS ON L1 DOOR AND R/H EMERGENCY DOOR EXIT SIGNS PER AMM 33-51-01. OPS CHECK GOOD.SDR SWAA2024122680903Sign · inoperativeL1 DOOR AND R/H MID EMERGENCY EXIT SIGN SEVERAL LAMPS INOP<[01] R&R SEVERAL LAMPS ON L1 DOOR AND R/H EMERGENCY DOOR EXIT SIGNS PER AMM 33-51-01. OPS CHECK GOOD.SDR SWAA2024122680438Battery · inoperativeEMERGENCY LIGHT BATTERY OVERWING (ROW 11DEF) INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT ROW 11DEF IN REFERENCE WITH AMM 33-51-06. OPS CHECK GOOD AT THIS TIMESDR SWAA2024121677654Seat Back · out of adjust12F SEAT BACK WONT STAY UPRIGHT<[01] SEAT BACK 12F LOCKED UPRIGHT. OK TO CONT PER MEL 25-6-02 SP1B AUTH #227755;[02] R/R SEAT 12F HYDROLOCK PER CMM 25-21-42. PERFORMED OPS CHECK OF PASSENGER SEAT BREAKAWAY (FWD & AFT) TO ALL OF THE EMERGENCY EXITS PER AMM 25-2SDR SWAA2024121675519Skin · crackedEXTERNAL POWER PLUG CUTOUT HAS A CRACK AT 6 O'CLOCK<[01] CUT AND REMOVED DAMAGE IN ZONE 2 PER SRM 53-10-15-2R-4;[02] PERFORMED VISUAL INSPECTION WITH 10X MAGNIFIER AND PERFORMED NDT PART 6 51-00-00 PROCEDURE 23 SURFACE INSPECTION ON CUT OUT AND INTERNAL SKIN; SDR SWAA2024121675484Battery Pack · failedM1675 FAILED CAPACITY CHECK<[01] R/R M1675 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06SDR SWAA2024121675485Battery Pack · failedM1674 FAILED CAPACITY CHECK<[01] R/R M1674 BATTERY PACK PER AMM 33-51-06SDR SWAA2024121675517Bracket · crackedL/H WING FWD ATTACH BRACKET FOR SUPPORT FOR PANEL 551BT IS CRACKED.<[01] REMOVED AND REPLACED BRACKET IAW SRM 51-40-02.SDR SWAA2024121075208Girt Bar · out of positionEMERGENCY SLIDE DOES NOT SEAT PROPERLY IN GUIDE ON FWD SVC DOOR<[01] REPOSITIONED GIRT BAR W/SIP. GIRT BAR NOW PROPERLY ENGAGES WITH STOW CLIPS.SDR SWAA2024112772249Probe · out of limits#2 ENGINE HIGHER THAN NORMAL EGT (630) WHILE AT IDLE AFTER ENG START. TEMP OF NUMBER #1 ENG WAS (480) WHICH IS MORE NORMAL. TEMP KBWI 50F. ON TAXI TOWER REPORTED TAIL PIPE FIRE #2 ENG.#2 ENG SHUTDOWN<[01] R&R #2 ENG T49.5 PROBE AND CJ9 HARNESS IAW AMM 77-21-01SDR SWAA2024112772258Harness · out of limits#2 ENGINE HIGHER THAN NORMAL EGT (630) WHILE AT IDLE AFTER ENG START. TEMP OF NUMBER #1 ENG WAS (480) WHICH IS MORE NORMAL. TEMP KBWI 50F. ON TAXI TOWER REPORTED TAIL PIPE FIRE #2 ENG.#2 ENG SHUTDOWN<[01] R&R #2 ENG T49.5 PROBE AND CJ9 HARNESS IAW AMM 77-21-01SDR SWAA2024111858895Battery Pack · inoperativeL2 EMERGENCY LIGHT INOP.<[01] RELAMPED; REF. AMM 33-51-04. NO FIX. SWAPPED POWER SUPPLIES M1672 AND M1673; REF. AMM 33-51-06. NO FIX. SWAPPED BACK TO ORIGINAL. CHECK CONTINUITY FROM D10746 TO GND; REF. WDM 33-51-14-6. GOOD CONTINUITY. REQUIRES MORE T/S; SHORT-SDR SWAA2024111859058Lens · out of adjustL2 EMERGENCY LIGHT LENS ASSEMBLY MISSING 1 SCREW.<[01] REPLACED MISSING SCREW IAW SIP.SDR SWAA2024110856318Girt Bar · misinstalledFORWARD ENTRY DOOR EMERGENCY SLIDE GIRT INCORRECTLY VELCROED TO BACKING PAN SHELF<[01] REMOVED FWD ENTRY DOOR SLIDE AND ADJUSTED SLIDE GIRT VELCRO AND REINSTALLED FWD ENTRY DOOR SLIDE PER MT 725-61-06.SDR SWAA2024110856314Skin · delaminatedREPLACE THE LH INBOARD MAIN FLAP DUE TO LOWER SKIN DELAMINATION<[01] REMOVED LH INBOARD MAIN FLAP PER MM 27-51-11;[02] 01 - INSTALLED LH INBOARD TRAILING EDGE FLAP PER [AMM 27-51-11-401-NG (INBOARD TRAILING EDGE FLAP - REMOVAL/INSTALLATION - PERMANENT)];[03] RSDR SWAA2024110656183Cover · missingCREW REPORTS AFT ENTERY DOOR EMERGENCY LIGTH COVER MISSING<[01] INSTALLED EMERGENCY LIGHT COVER AT AFT ENTERY DOOR REF B737 AMM 33-51-01SDR SWAA2024110656113Skin · delaminatedFLT CREW REPORTS LEFT INBD FLAP; AFT OTBD CORNER DELAM<[01] C/W EA 24-157-03032 TSR#2024007736SDR SWAA2024102852640Power Supply · inoperativeEMERGENCY LIGHTS AT ROWS 7ABC; 9ABC; AND 14ABC INOP.<[01] R&R EMERGENCY POWER SUPPLY AND BATTERY PACK M2335 REF AMM 33-51-06. OPS GOOD.SDR SWAA2024102854223Battery Pack · inoperativeEMERGENCY LIGHTS AT ROWS 7ABC; 9ABC; AND 14ABC INOP.<[01] R&R EMERGENCY POWER SUPPLY AND BATTERY PACK M2335 REF AMM 33-51-06. OPS GOOD.SDR SWAA2024102452133Seat Back · out of adjustSEAT 11FRECLINES INTO EXIT ROW<[01] ADJUSTED HYDROLOC TO INHIBIT EXIT ROW RECLINE PER AMM25-22-00SDR SWAA2024101448456Drain · leakingFUEL DRIP ON #2 ENG RAN ENGINE; PER MX FOR 5 MIN & ENGINE CONTINUED TO DRIP<[01] RAN ENGINE FOR 5 MINUTES & FOUND THE MAIN FUEL PUMP DRAIN LEAKING 7 DROPS PER MINUTE & FOUND TO BE WITHIN THRESHOLD LIMITS WITH NO MX ACTION NECESSARY PER AMM 71-71-00. A/C OK FORSDR SWAA2024101447415Retainer · out of adjustGIRT BAR DOESNT STAY IN PLACE WHILE OPENING L1 DOOR<[01] ADJUSTED RETENTION OF GIRT BAR RETAINER CLIPS IAW SIP. CLIPS AND GIRT BAR FUNCTION AS NORMAL. NO DEFECTS NOTED AT THIS TIME.SDR SWAA2024101147454Slide · dislodgedL1 DOOR SLIDE FELL OUT OF BUSTLE.<[01] REINSTALLED L1 DOOR SLIDE PER MT725-61-06.
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