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 SWAA2021121343326Structure · corrodedRT OVERWING EMERGENCY EXIT CUTOUT STRUCTURE IS CORRODED ON THE LWR SILL, BS 635-619 RBL 71. SIX RIVETS REMOVED FOR ACCESS IAW SRM 51-40-02-0G-0. CORROSION REMOVED EMERGENCY EXIT CUTOUT STRUCTURE LOWER SILL WEB IAW SRM 51-40-15-1A-1, DAMAGE ALLOWED 1 PARAGRAPHSDR SWAA2021121343327Support Angle · corrodedRT OVERWING EMERGENCY EXIT CUTOUT SUPPORT ANGLE IS CORRODED ON THE LWR SILL; BS 627; RBL71. REMOVED SUPPORT ANGLE LOCATED BTW BS 620-634 RBL 71 IAW SRM 51-40-02-0G-0. NO ENTRIES ALLOWABLE DAMAGE IN SRM MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; PASDR SWAA2021121343315Stiffener · crackedRIGHT HORIZONTAL STAB INSPAR RIB HSS 111.10, 4TH VERTICAL STIFFENER IS CRACKED. EDDY CURRENT INSPECTED 4TH VERTICAL STIFFENER IAW NDT MANUAL PART 6, 51-00-00, PROCEDURE 23. CRACKING INDICATION NOTED APPROXIMATELY .75 INCH FROM BOTTOM OF RIB ON STIFFENER APPRSDR SWAA2021121343319Stiffener · crackedRIGHT HORIZONTAL STABILIZER INSPAR RIB HSS 120.30. 3RD VERTICAL STIFFENER IS CRACKED. REMOVED DAMAGED PART OF THE RIB HSS 120.3 STIFFENER. CUT OUT ON WEB 0.5' X 0.250' IAW SRM 55-10-09-2R-4. HFEC INSPECTED CUT OUT IAW NDTM PART 6 51-00-00, PROCEDURE 23, NOSDR SWAA2021121343322Panel · pulledRT WING T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES. CLEANED PANEL AND REMOVED FINISH AS NEEDED IAW AMM 51-21-11-150-815 PARA. 17. C. AND D. VISUAL INSPECTION FOUND DAMAGE TO GLASS FIBER PLIES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4. SDR SWAA2021121342883Panel · elongatedLT WING T/E PANEL 561BB HAS ELONGATED HOLE ON L/E (MARKED) ; / [01] PART/MATERIAL IDENTIFIED PER SRM 57-51-01-0I-1 FIG 3 TABLE 3 ITEM 9 . ELONGATED FASTENER HOLE ON THE EDGE BAND EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-51-01-1A-1 PARA 4 B. <BR>REPAIR TSDR SWAA2021121343272Skin · crackedCRACK AROUND THE FASTENER AT NO.8 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. EDDY CURRENT INSPECTED AREA IAW NDT MANUAL PART 6; 51-00-00 PROCEDURE 23. EXTENT OF CRACK NOTED APPROXIMATELY .100 INCHES IN LENGTH. INSTALLED REPAIR PARTS IAW SDR SWAA2021121343273Skin · crackedCRACK AROUND THE FASTENER AT NO.5 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. EDDY CURRENT INSPECTED AREA IAW NDT MANUAL PART 6; 51-00-00 PROCEDURE 23. EXTENT OF CRACK NOTED APPROX .100 INCHES. REMOVED DAMAGED PART IAW SRM 57-42-01-2R-8, STSDR SWAA2021121343274Panel · crackedPANEL 561BB HAS NUMEROUS CRACKED PULLED THROUGH SEAL FASTENER HOLES ON T/E. EXCEED ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4 B. REPAIR TO BE PERFORMED IAW SRM 51-70-05-2R-9, SRM 57-51-01-2R-1 PARA 4 D TABLE 202. PERFORMED DAMAGE REMOVAL & SURFACE PREPSDR SWAA2021101830477Slide · detachedFRONT ENTRY EMERGENCY SLIDE DETACHED FROM ITS COMPARTMENT AFTER FLIGHT ATTENDANT CORRECTLY SECURED GIRT BAR FROM ITS ARMED POSITION. FRONT ENTRY DOOR WAS UNABLE TO BE FULLY OPENED ; / [01] CW MT 725-61-06SDR SWAA2021100826541Girt Bar · displacedCREW REPORTS FWD SERVICE DOOR SLIDE GIRT BAR DISPLACED. ; CREW REPORTS FWD SERVICE DOOR SLIDE GIRT AR DISPLACED. / [01] RESECURED GIRT BAR IAW SIP. AIRCRAFT OK FOR SERVICESDR SWAA2021100525280Slide · out of toleranceCREW REPORTS FWD ENTRY DOOR ESCAPE SLIDE OUT OF GREEN BAND. ; / [01] R&R SLIDE PER MT#725-61-06-FESDR SWAA2021100524325Lens · missingFWD GALLEY 'EXIT LIGHT' LENS MISSING. ; / [01] FOUND AND REINSTALLED EXIT LIGHT LENS AT FWD. GALLEY (G1) IAW BOEING 737-700 AMM 33-51-01-960-802-NG.; [02] VERIFIED STEP 1.SDR SWAA2021092823522Light · inoperativeEMERGENCY EXIT AISLE LIGHTS AT SEAT ROWS 9CBA AND 17CBA ARE INOP ; / [01] REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF EMERGENCY EXITS AISLE LIGHT LAMPS AT SEAT ROWS 9CBA AND 17CBA PER AMM 33-51-03-960-801; [02] VERIFIED REMOVED; REPLACED AND PERFSDR SWAA2021092823095Battery Pack · inoperativeRIGHT OVERDOOR EXIT SIGN DOES NOT ILLUMINATE; OTHER LIGHTS RELATED TO M1675 BATT PACK OPERATE CORRECTLY. ; / [01] FOUND 7822 CAME IN WITH D40042J CONNECTOR PART NUMBER BACC65AK221P SHOULD BE BACC65AK211P PER WDM EQUIPMENT LIST. CONNECTOR DID NOT MATE PROPERLY SDR SWAA2021100522656None · crackedLH AND RH OVERWING EXIT GRIP ASSY PN- 65C35987-5 CRACKED / [01] REMOVED AND REPLACED LH AND RH OVERWING EXIT GRIP ASSY AS PER SOPM 20-50-01; [02] CERTIFIED; [03] VERIFIED STEP 1/2SDR SWAA2021092823094Light · inoperativeLEFT EMERGENCY LIGHTING SYSTEM GROUND ILLUMINATION LIGHT DOES NOT ILLUMINATE ; / [01] RELAMPED LEFT GROUND ILLUMINATION LIGHT; LIGHT STILL DOES NOT ILLUMINATE PER TASK 33-51-04-960-801<BR>.; [02] VERIFIED RELAMPED LEFT GROUND ILLUMINATION LIGHT; LIGHT STILL DOSDR SWAA2021100518395Rib · crackedLH HORIZONTAL STAB L/E ACCESS PANEL RIB 4 HAS A CRACK. ; / [01] REMOVED CRACKED RIB P/N 186A1304-1 PER B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED RIB REMOVAL; [03] LOCATED AND DRILLED NEW RIB P/N 186A1304-1 PER B737-700 SRM 51-10-02-0G-0.; [04] VERIFIED DRILLISDR SWAA2021100518396None · crackedLH HORIZONTAL STAB L/E ACCESS PANEL RIB 5 HAS A CRACK. ; / [01] REMOVED RIB #5 AT LH HORIZONTAL STAB L/E ACCESS PANEL AS PER B737-700 SRM 51-40-02 -0G-0; [02] REMOVED RIB CRACKED P/N 186A1305-1 AT LH HORIZONTAL STAB PANEL AS PER B737-700 SRM 51-40-02-0G-0; [03SDR SWAA2021092017606Slide · looseFORWARD SERVICE DOOR SLIDE HAD STARTED TO UNPACK FROM CONTAINER ; / [01] RE-SECURED SLIDE IN COMPARTMENT PER TASK CARD MT 725-61-06SDR SWAA2021100517048Skin · delaminatedL1 DOOR UPPER AFT CORNER SKIN LIFTED ; / [01] REMOVED 1 EA FASTENER ON L1 DOOR AFT CORNER OUTER SKIN FOR REWORK AND NDT PER B-737-7 SRM 51-40-02-0G-0; [02] VERIFIED REMOVAL.; [03] REWORKED AND STRAIGHTENED AFT CORNER SKIN PER BAC5300-2 STEP 8.2.1; [04] VERIFIESDR SWAA2021100416010Angle · crackedSUPPLEMENTAL INFORMATION: AFT CARGO BAY ANGLE CRACKED BS 867 LBL 15 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] LOCATED AND DRILLED ANGLE BS 867 LBL 15 WL 156; OK TO INSTALL PER SRM 51-40-02-0G-0 AND DWG 149A8102; [03] REMOVED CRACKED CLIP BS 867 LBL 15 WL 156 SDR SWAA2021100515051None · corrodedREF TTG8Q0068VX9 CABIN FLOOR SUPPORT BEAM TOP CAP HAS LIGHT CORROSION AROUND NUT PLATE HOLES AT BS 986.5 32' RIGHT OF CENTER LINE- COMPLIANCE FINDING WRONG ATA AND MEASUREMENTS CORRECTION ; REF TTG8Q0068VX9 CAIN FLOOR SPPORT EAM TOP CAP HAS LIGHT CORROSION AROSDR SWAA2021090914905Lamp · inoperativeEMERGENCY LIGHT AT 20 ABC INOP ; / [01] RELAMPED EMERGENCY AREA LIGHT AT 20ABC IAW AMM 33-51-03.SDR SWAA2021100414512Support · damagedACB R/H FLOOR TO SIDEWALL SUPPORT BS 887-947 HAS OVERSIZED HOLES AT SPLICE LOCATION BS 887 RBL 25 WL 156 ; / [01] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS887 - BS947; RBL25; WL156 PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED ACB FLOOR TO SIDEWALL SUPPORTSDR SWAA2021100414172Support Angle · crackedFWD CARGO BAY BULKHEAD R/H SIDEWALL SUPPORT ANGLE AT 500D LOWER FLANGE I/B FASTENER HOLE ELONGATED ; / [01] ELONGATED HOLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS; [03] REMOVED FWD CARGO BAY BULKHEAD SUPPORTSDR SWAA2021100414170Support Angle · elongatedFWD CARGO BAY BULKHEAD L/H SIDEWALL SUPPORT ANGLE AT 500D LOWER FLANGE I/B FASTENER HOLE ELONGATED ; / [01] ELONGATED HOLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS; [03] REMOVED FWD CARGO BAY BULKHEAD SUPPORTSDR SWAA2021090713797Scuff Plate · crackedFORWARD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED CRACKED FCB AFT CORNER SCUFF PLATE PER SRM 53-30-15-2R-1 PARA 4. B.(2) AND (4) ACCOMPLISHED FPI INSPECTION TO SCUFF PLATE IAW BOEING SOPM 20-20-02. NO CRACKS NOTED. SANDED REPAIR WELD AREA IAW SRM 5SDR SWAA2021090313321Panel · puncturedFAIRING PANEL 193B PANEL SCREW HOLES ELONGATED AND INNER SURFACE PUNCTURED ; / [01] R&R CENTER WING TO BODY PANEL 193B PER AMM 53-51-21.SDR SWAA2021100512758Seat Track · crackedCRACK NOTED ON LBL24.75 POSITION 'B' HOLE ; CRACK NOTED ON SEAT TRACK BS 727B LBL24.75 POSITION 'B' HOLE; CRACK LENGTH 0.030' / [01] ACCOMPLISHED FIRST OVERSIZE CLEANUP REAM TO FASTENER HOLE TO A MINIMUM OF 0.016' AS PER REFERENCE NDT PART 6; 51-00-00; PROCEDUSDR SWAA2021100512760Seat Track · crackedCRACK NOTED ON SEAT TRACK BS 727B LBL45.5 POSITION 'B' HOLE; CRACK LENGTH 0.030' ; CRACK NOTED ON SEAT TRACK BS 727B LBL 45.5 POSITION 'B' HOLE; CRACK LENGTH 0.030' / [01] ACCOMPLISHED FIRST OVERSIZE CLEANUP REAM TO FASTENER HOLE TO A MINIMUM OF 0.016' AS PER SDR SWAA2021100512753Splice Strap · corrodedCORROSION FOUND AT AFT CARGO FLOOR BOARD SPLICE STRAP AT STA 767 + 5. ; / [01] REMOVED CORROSION AT AFT CARGO FLOOR BOARD SPLICE STRAP STA 767.5 AS PER REF B737 SRM 51-10-02-0G-0.; [02] VERIFIED. REMOVED CORROSION AT AFT CARGO FLOOR BOARD SPLICE STRAP STA 767.SDR SWAA2021100412687Attach Angle · crackedSEAT TRACK ATTACH ANGLE FOR SADDLE CRACKED BS 500D-520 LBL 45 WL205 ; / [01] LOCATED AND DRILLED HOLES ON NEW SEAT TRACK ANGLE FOR SADDLE BS 500D-520 LBL 45 WL 205 IAW SRM 51-40-05 AND DWG 143A5410 ID:0013 REV:B.; [02] CORRECTION FOR CORRECT DWG: DWG 143A5034 SDR SWAA2021100412686Panel · crackedPANEL 191AL INNER SURFACE; FWD LOWER CORNER IS CRACKED AT CORE ; / [01] IDENTIFIED PANEL 191AL IAW SRM 53-30-70-0I-1.FIG 2; ITEM [1]. FOUND DAMAGE AT 3' FROM FWD EDGE; 2'FROM LOWER EDGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-30-70-1A-1.PARA 4.A.(1). REQUIRESSDR SWAA2021100411990Intercostal · corrodedCORROSION ON INTERCOSTAL AT B.S. 500D+1; L.B.L. 7; W.L. 151. ; / [01] CORROSION ON INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-04-1A-1 FIGURE 102 DETAIL E.; [02] VERIFIED DAMAGE OUT LIMITS PER SRM 53-00-04-1A-1; [SDR SWAA2021100411993Stringer · crackedCRACK ON END OF STRINGER 26 LEFT B.S. 520+17. ; / REMOVED DAMAGED AREA S-26L BS 500D+10'-540 IAW SRM 53-00-03-2R-1 REP.1; [02] REQUIRED NDI INSPECTION S-26L BS 500D+10' CUT OUT CRACK FREE IAW SRM 53-00-03-2R-1 REP.1 RECEIVED STR REPAIR SECTION FROM OSS FABRICASDR SWAA2021100410765None · corrodedCORROSION ON BS 986 FLOOR BEAM UPPER CHORD LBL 44 WL 208 ; / [01] WORK COMPLETED ON CARD NO. M-21-153-00612 (2529).; [02] VERIFIED WORK COMPLETED ON CARD NO. M-21-153-00612 (2529).SDR SWAA2021100410768None · crackedCRACKED UPPER ANGLE ON SUPPORT WEB BS 927-947 BL 0 WL 208 ; / [01] REMOVED UPPER ANGLE FROM WEB SUPPORT BS 927-947 BL 0 WL 208 PER SRM 51-40-02; [02] LOCATED AND DRILLED NEW UPPER ANGLE ON SUPPORT WEB BS 927-947 BL 0 WL 208 PER SRM 51-40-05-0G-0 AND DWG 147A54SDR SWAA2021100410764None · corrodedCORROSION ON BS 986 FLOOR BEAM UPPER CHORD RBL 44 WL 208 ; / [01] REMOVED CORROSION ON BS986 FLOOR BEAM UPPER CHORD RBL44 WL208 IN AREA OF 0.9' BY 1.1' BY A DEPTH OF 0.065' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1.; [02]SDR SWAA2021092810770Intercostal · crackedCRACKED FLOOR SUPPORT BS 277-294 BL 0 WL 208 ; / [01] REMOVED CRACKED SUPPORT AT BS 277-294 BL0 WL 208; LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-02 SRM 51-40-05. REQUEST OKAY TO INSTALL; [02] VERIFIED REMOVED CRACKED SUPPORT AT BS 277-294 BL0 WL 208; LOCASDR SWAA2021092810771Intercostal · crackedCRACKED FLOOR SUPPORT BS 344-360 BL 0 WL 208 ; / [01] ET INSPECTED SUSPECTED CRACK IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK EXISTS.<BR>CAL ID IS000450 N500D; [02] REMOVED INTERCOSTAL AT BS344-360 BL0 WL 208; PER SRM 51-40-02. LOCATED AND DRILLSDR SWAA2021100510843None · looseL1 DOOR ESCAPE SLIDE GIRT BAR AFT CLIP IS NOT SECURED. MOUNTED ON THE ESCAPE SLIDE CONTAINER. ; / [01] RESECURED GIRT BAR AFT CLIP;MOUNTED ON THE ESCAPE SLIDE CONTAINER;AT L1 DOOR.PER B 737-700 SRM 51-40-02-OG-0.; [02] VERIFIED RESECURED GIRT BAR AFT CLIP;MOUNSDR SWAA2021100510838None · crackedRH Z CHANNEL BETWEEN STA 500 AND STA 500A HAS CRACKED ; / [01] REPLACED FWD CARGO R/H Z CHANNEL BETWEEN STA 500 THRU 500A REF.B737-700 SRM 51-40-02-0G-0. CHANNEL WILL BE INSTALLED ON FWD CARGO MOC. CARD #TTG8Q004GCN6; [02] VERIFIED NEW PART AND TTG8Q004GCN6 FOSDR SWAA2021100510833Scuff Plate · crackedAFT CARGO COMP. AFT CORNER SCUFF PLATE CRACKED ; / [01] LOCATED AND DRILL NEW AFT CARGO AFT SCUFF PLATE AS PER REF B737-700 SRM 51-41-05-0G-0; [02] REMOVED AFT CARGO AFT CORNER SCUFF PLATE AS PER REF B737-700 AMM 53-11-02-020-801; [03] VERIFIED STEPS #1 AND #2SDR SWAA2021100510835None · corrodedRH Z CHANNEL SUPPORT STA 495 TO STA 500A HAS SPOTS OF CORROSION. ; / [01] FWD CARGO R/H SIDE Z CHANNEL (SHIELD ASSY) WAS REPLACED ON FAULT #TTG8Q0068W71; [02] VERIFIED Z CHANNEL REPLACEMENTSDR SWAA2021100410728Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 847; LBL 22; WL 154 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] VERIFIED CORROSION ON SUPPSDR SWAA2021100410745Shield · corrodedCORROSION ON AFT CARGO BAY DOOR CUT-OUT FWD SHIELD FROM STA 767 TOO STA 787+7; RBL22; WL 154 ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TSDR SWAA2021100410729Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STA 867+15; RBL 22; WL 157 ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D.; [02] VERIFIED CORROSION OUT OF LIMITS SDR SWAA2021100410727Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 767; RBL 22; WL 154. ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLE PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] UPDATED STATEMSDR SWAA2021100410712Bracket · cracked#1 ENGINE O/B T/R AFT FIRE SEAL LABRYNTH BRACKET ON PYLON IS CRACKED ; #1 ENGINE O TR AFT FIRE SEAL LARYNTH RACKET ON PYLON IS CRACKED / [01] REMOVED AND REPLACED #1 ENG O/B T/R AFT FIRE SEAL LABRYNTH BRACKET ON PYLON PER SRM 51-40-02-0G-0 STEP 4. AND PER IPC
Back to Boeing 737-76N