Boeing 737-73V
Service difficulty reports · 1,826
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 = '73773V' 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 = '73773V' 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 SWAA2022032363876Frame · crackedDURING INSPECTION OF LEFT HAND PICKLEFORK PER EA 1-A53-35829 REV IR; DAMAGE (CRACK) WAS FOUND AT LOWER LEFT SIDE AS DEPICTED IN FUGURE 1 AREA 'C' ON EA / THE L/H PICKLEFORK FRAME WAS REMOVED AND REPLACED ON BOEING AOG AGREEMENT SWA-RE-1906934. REF SWA EA 1-753SDR SWAA2022040863863Fitting · crackedDURING INSPECTION OF BS 663.7 FRAME FITTING CRACKS WERE FOUND ON LHS AND RHS FRAME FITTINGS AS WELL AS THE LHS FAIL SAFE STRAP STA 663.75. REF: EA 1-753-35798 REV 1 / THE LH PICKLE FORK FRAME P/N 144A2410-7 & FAIL SAFE STRAP P/N 144A2412-1. THE RH PICKLE FORK SDR SWAA2022040663860Frame · crackedL/H PICKLE FORK FITTING AND FAIL - SAFE STRAP ARE CRACKED AT THE LOWER AFT FASTENER AND CRACK EXTENDS PAST THE FASTENER; LOCATED AT BS 663 / THE LH PICKLE FORK FRAME P/N 144A2410-7 & FAIL SAFE STRAP P/N 144A2412-1 WAS REMOVED AND REPLACED BY BOEING AOG UNDER ASDR SWAA2022040663859Frame · crackedR/H PICKLE FORK IS CRACKED AT THE LOWER AFT FASTENER CRACK DOES NOT EXTEND PAST THE FASTENER; LOCATED AT BS 663 / THE RH PICKLE FORK FRAME P/N 144A2410-8 & FAIL SAFE STRAP P/N 144A2412-2 WAS REMOVED AND REPLACED BY BOEING AOG UNDER AGREEMENT SWA-RE-1906934 IN SDR SWAA2019100937707Bushing · missingL2 DOOR SLIDE GIRT BAR RETAINING BUSHING MISSING. INSTALLED BUSHING PER AMM & SIP.SDR SCNA2019100197177Connector · dirtyLEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED BETWEEN 5-15 PERFORMED QRH 9.14. CREW INITIATED GO AROUND AND DECLARED EMERGENCY, AND FLIGHT LANDED SAFELY ON SECOND APPROACH. PERFORMED FIM TASK 27-51 #830, TASK #803 & TASK 820. PERFORMED LEADING EDGE CONTROL SYSTESDR SCNA201910019183Skin · wornRH LE SLAT #7 BARE METAL SHOWING ON UNDERSIDE ALONG AFT EDGE. FOUND TRAILING EDGE WEAR BEYOND REPAIRABLE LIMITS PER SRM 57-42-01-2R-6 REPAIR 6. REMOVED #7 SLAT REF AMM 27-81-21. INSPECTED INTERFACE, OK TO INSTALL. INSTALLED NEW SLAT IAW AMM 27-81-21-400-801. SSDR SCNA2019100194182Structure · worn#1 SLAT UNDER TRAILING EDGE HAS WORN ANTI ABRASION PAINT NUMEROUS SPOTS. OUTBOARD TRAILING EDGE WEAR IS BEYOND ALLOWABLE LIMIT AND WILL REQUIRE REPAIR PER SRM 57-42-01-2R-6 REPAIR 6. REPAIRED REF SRM 57-42-01-2R-6SDR SCNA2019100194181Skin · damagedRH LE SLAT #6 BARE METAL SHOWING ON UNDERSIDE ALONG AFT EDGE. FOUND TRAILING EDGE WEAR BEYOND SRM REPAIRABLE LIMITS PER SRM 57-42-01-2R-6 REPAIR 6. REMOVED #6 SLAT REF AMM 27-81-21. PERFORMED INTERFACE INSPECTION AND OK TO INSTALL NEW SLAT. INSTALLED NEW SLAT SDR SCNA2019100194180Structure · corrodedAFT CARGO DOOR, CORROSION ON LOWER AFT INSIDE CORNER NEXT TO INSULATION BUTTON. SEE SRM 52-30-01/1A01 FOR LIMITS. METAL THICKNESS .071 MATERIAL 7075T6. REMOVED CORROSION AT 2 LOCATIONS WITH CUTOUTS AT LOWER AFT CORNER AND LOWER INNER SKIN FWD OF AFT STOP FITTISDR SCNA2019100192179Fastener · looseLEFT WING, UPPER L/E 16 LOOSE FASTNERS FROM THE PYLON INBD. ALONG THE AFT SIDE OF PANEL. REMOVED 16 EA LOOSE FASTENERS ON L/H WING UPPER SKIN JUST INBD OF # 1 PYLON. REAMED HOLES TO 1ST OVER 3/16. .199" OPEN HOLE AND COUNTER SINK HFEC ACCOMPLISHED BY NDI. NO CSDR SCNA2019100194178Spar · cracked11" CRACK ON WING CENTER SECTION REAR SPAR BETWEEN 45.64 AND 31.83 STIFFENERS. COMPLETED INTERIM REPAIR IAW SRM 57-10-10-2R-2 PARAGRAPH 6. ITEM WILL BE PLACED ON GMM/MTI FOR TRACKING PURPOSES FOR A DETAILED VISUAL INSPECTION EVERY 3,000 FLIGHT CYCLES. IF ADDITSDR SWAA2019092437155Actuator · out of adjustFUEL IMBALANCE OF 1,000 LBS. IN 15 ON DESCENT. LEFT WING LOW. ADJUSTED CROSSFEED VALVE ACTUATOR IAW AMM.SDR SWAA2022032112163Bracket · brokenPANEL 192E NUTPLATE FORWARD SUPPORT BRACKETS BROKEN / REMOVED AND REPLACED PER SRM 51-40-02SDR SWAA2019091937055Splice · brokenOVERWING EXIT LIGHT ASSY SPLICE DAMAGED. REPAIRED SPLICE REF SWPM AND AMM.SDR SCNA20190907176Screw · unsecure#3 SPOILER DAMAGED DUE TO SCREW POPPED OUT FROM THE TRAILING EDGE OUTBOARD FLAP. REMOVED #3 SPOILER IAW AMM 27-61-11. INTERFACE INSPECTION OF #3 SPOILER COMPLIED WITH, OK TO INSTALL. INSTALLED #3 SPOILER IAW AMM 27-61-11. PERFORMED SPOILER SYSTEM TEST AND ADJUSDR SCNA20190907175Skin Panel · wornRIGHT WING OUTBOARD TRAILING EDGE MAIN FLAP TOP PANELS ARE WORN. REMOVED OUTBOARD TRAILING EDGE FLAP PER AMM 27-51-21-000-801. INTERFACE INSPECTION OF RT OTBD TRAILING EDGE FLAP AND AFT FLAP SECTION COMPLIED WITH. OK TO INSTALL. INSTALLED RT OB FLAP REF AMM 27SDR SCNA20190907174Screw · brokenTE OB FWD FLAP DAMAGED DUE TO SCREW BROKEN FROM 10FT OB OF THE FLAP. DAMAGE PAST LIMITS FOR SRM 57-53-01-01-03. REMOVED LT OUTBOARD FLAP PER AMM 27-51-22. INSTALLED SERVICEABLE LT OB MAIN FLAP REF AMM 27-51-21-400-801. FLAP ADJUSTMENT PERFORMED PER AMM 27-51-2SDR SCNA20190907173Intercostal · crackedTHE WEB LOCATED AT EMPENAGE STATION 1040 HAS A .6 INCH LONG CRACK AT THE MOST LEFT LIGHTENING HOLE. DRILLED A .128" DIA STOP HOLE AT END OF CRACK. OPEN HOLE NDT ACCOMPLISHED AND NO CRACK BEYOND STOP DRILL HOLE. REMOVED DAMAGE FROM INTERCOSTAL WEB IAW SRM 53-00SDR SWAA2019091236845Fastener · looseL2 DOOR SLIDE HAD A LOOSE FASTENER. SECURED FASTENER PER SIP.SDR SWAA2022031566043Skin · crackedNUMBER 7 LEADING EDGE SLAT OUTBOARD SKIN TAB IS CRACKED. / REMOVED AND REPLACED NUMBER 7 LEADING EDGE SLAT OUTBOARD SKIN TAB IAW SRM 51-40-02.SDR SWAA2019080635665Battery Pack · inoperativeR1 DOOR EMERGENCY LIGHT INOPERATIVE. / R&R BATTERY PACK M1675 IAW AMM.SDR SWAA2019080635577Battery Pack · inoperativeAFT OF R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.SDR SWAA2019080635576Battery Pack · inoperativeDOORWAY EMERGENCY LIGHT MODULE INOPERATIVE. R&R BATTERY PACK M1675 IAW AMM.SDR SWAA2019080135487Bulkhead Web · crackedLOWER VAPOR BARRIER CRACKED AT BS. 663, LBL 46. / REPAIRED LOWER VAPOR BARRIER IAW SRM.SDR SWAA2019072935357Light · inoperativeRT OVERWING ESCAPE HATCH LIGHT L751 INOP. RELAMPED LIGHT L751 PER AMM.SDR SWAA2022031411614Vapor Barrier · crackedR/H MAIN WHEEL WELL; LOWER VAPOR BARRIER CRACKED / APPLIED REPAIR PATCH CLOTH OVER CRACKED AREA IN R/H MAIN WHEEL WELL LOWER VAPOR BARRIER (#120) LOT# 5076276-1 IAW SRM 57-10-10-2R-2 STEPS 6(A-D) APPLIED BMS 5-95 (B 1/2 SEALANT) AT 12:45PM ON 27JUL19 56800U 27SDR SWAA2022031411440Seal · crackedRT UPPER FWD SLIDER SEAL CRACKED / R&R RT HORIZONTAL STAB. UPPER FWD SLIDER SEAL REF AMM 53-31-31.SDR SWAA2019072535304Battery Pack · failedEMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PACK PER AMM.SDR SWAA2019072535280Battery Pack · failedEMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PACK PER AMM.SDR SWAA2019072535276Lens · crackedOVERWING CEILING EXIT SIGN LENS CRACKED. R&R LENS IAW AMM.SDR SWAA2022031163909Seal · crackedLH HORIZONTAL STABILIZER UPPER FWD SLIDER IS CRACKED / R&R LH HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL REF AMM 53-31-31.SDR SWAA2022031163910Seal · crackedRH HORIZONTAL STABILIZER UPPER FWD SLIDER IS CRACKED / REMOVED AND REPLACED RH HORIZONTAL STABILIZER UPPER FWD SLIDER PER MM 53-31-31SDR SWAA2019071834952Battery · failedEMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER AMM.SDR SWAA2019071634828Battery Pack · failedEMERGENCY BATTERY POWER SUPPLY M1672 FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.SDR SWAA2022031165276Strap · corroded***CORROSION*** ON STRAP COMMON TO HORIZONTAL WEB; AT S-23L; BS294.5 + 22'; E/E COMPARTMENT. / REPAIRED PER: EA 1-753-35284; REV IR AND ATS ER 19-03997; REV IR.SDR SWAA2019071734899Shear Tie · corrodedVERTICAL WEB OUTBOARD FORWARD SHEAR TIE ANGLE CORRODED AT BS. 294.5+24, STR. 23L. R&R ANGLE IAW SRM AND DWG.SDR SWAA2019071734898Web · corrodedVERTICAL WEB FORWARD CORRODED AT BS. 294.5+24, STR. 23L. R&R WEB IAW SRM AND DWG.SDR SWAA2019071734897Web · corrodedHORIZONTAL WEB CORRODED ON UPPER SURFACE BETWEEN BS. 316.5 TO BS. 321.5, STR. 23L. R&R WEB IAW SRM & DWG.SDR SWAA2019070934678Fitting · crackedCARGO BAY INTERCOSTAL TO FRAME CLIP CRACKED AT BS. 500C, LBL 25. R&R FRAME CLIP IAW DWG & SRM.SDR SWAA2022031165263Angle · crackedBS 947 LBL 10 WL 156 WATER TANK SUPPORT ANGLE CRACKED / REMOVED ACB WATER TANK SUPPORT ANGLE BS947; LBL10 PER SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW WATER TANK SUPPORT ANGLE PER DWG 149A8103; AND SRM 51-40-05-0G-0. OK TO INSTALL 87713U 10JUL19 1035C 10JUL19SDR SWAA2022031165261Skin · corrodedCORROSION ON SKIN AND FROM BS 896-1002 APPROS STR 2L -2R UNDER FOOT PRINT OF DORSAL FIN / REMOVED CORROSION ON CROWN SKIN BETWEEN BS 896 TO BS 1002 STR 2L TO 2R. ALL BLENDED AREAS WERE FOUND TO BE WITHIN THE LIMITS PER SRM 737-700 ALLOWABLE DAMAGE FIG 103; DETSDR SWAA2022031165224Seal · crackedLT HORIZ. STAB FWD UPPER SLIDE SEAL IS CRACKED. / REMOVED & REPLACED LT HORIZ STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-000-801 & AMM 53-31-31-400-801 56304U 09JUL19SDR SWAA2022031165225Seal · crackedRT HORIZ. STAB FWD UPPER SLIDE SEAL IS CRACKED. / REMOVED & REPLACED RT HORIZ. STAB FWD UPPER SLIDE SEEL IAW AMM 53-31-31-000-801 & AMM 53-31-31-400-801 56304U 09JUL19SDR SWAA2022031165241Gusset · crackedFWD CARGO BAY 500D GUSSET IS CRACKED STR 19L/H / REMOVED GUSSET B.S. 500D STR 19 L/H PER SRM 51-40-02-0G-0 DRILLED AND LOCATED GUSSET PER SRM 51-40-05; OK TO INSTALL 556823R INSP 18 2JUL19 INSTALLED GUESSET PER SRM 51-40-02-0G-0 AND DWG 143A7902SDR SWAA2022031165242Gusset · crackedFWD CARGO BAY 500D GUSSET IS CRACKED STR 19R/H / REMOVED GUESSET B.S. 500D STR19 R/H PER SRM 51-40-02-0G-0 DRILLED AND LOCATED GUSSET PER SRM 51-40-05. OK TO INSTALL 56823R 02JUL19 INSP 18 2JUL19 INSTALLED GUSSET PER SRM 51-40-02-0G-0 AND DWG 143A7902SDR SWAA2022031165246Angle · crackedACB ANGLE CRACKED BS 867 LBL 18 / REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE AT BS 867 LBL18 WL156 IAW SRM 51-40-02 AND DWG 149A8102SDR SWAA2022031165254Angle · crackedACB BULKHEAD ANGLE CRACKED BS 727+4 RBL 3 / REMOVED & REPLACED THE BULKHEAD ANGLE ACB BS 727+4 RBL 3 INSTALLED PER DWG 144A2600SDR SWAA2022031165248Strip · corroded***CORROSION*** ACB NUTPLATE STRIP IS CORRODED BS 787 - 794 RBL 18WL / REMOVED CORRODED NUTPLATE STRAP AND ISTALLED NEW NUTPLATE STRAP AT BS 787-794 RBL18 WL156 IAW SRM 51-40-02 AND DWG 146A0081SDR SWAA2022031165247Strip · corroded***CORROSION*** ACB NUTPLATE STRIP IS CORRODED BS 794 TO 803 RBL 18 WL 156 / REMOVED CORRODED NUTPLATE STRAP AND INSTALLED NEW NUTPLATE STRAP AT BS 794-803 RBL18 WL156 IAW SRM 51-40-02 AND DWG 146A0081
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