N8652B
Service difficulty reports · 163
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N8652B' AND registry_match = 'registration' 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 n_number = 'N8652B' AND registry_match = 'registration' 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 SWAA2022092647779None · corrodedFWD GALLEY DOOR CUTOUT LOWER THRESHOLD 'L' ANGLE HAS CORROSION AT 5EA FASTENER HOLE LOCATION. (MARKED) / [01] REMOVED DAMAGE I.A.W SRM 51-10-01. MEASURED DAMAGE DEPTH TO BE .019? IN DEPTH. DAMAGE DEPTH FOUND TO BE BEYOND ALLOWABLE LIMITS AS GIVEN IN SRM 53-10-SDR SWAA2022092247805Angle · crackedAFT CARGO STA. 867 LBL-12; LAV. TANK POST LOWER ATTACH CLIP/ANGLE CRACKED. / [01] REMOVED LOWER ATTACH ANGLE (BRACKET).;[02] REMOVED AND REPLACED BRACKET IAW SRM 51-40-02.;[03] REMOVED AND REPLACED BRACKET IAW SRM 51-40-02. C/W INSPECTIONSDR SWAA2022092647074Scuff Plate · crackedAFT CARGO DOOR FWD SCUFF PLATE CRACKED AT STA 787 AFT CARGO DOOR FWD SCUFF PLATE P/N: 81205-146A8341-7 AT STA 787 CRACKED. / [01] REMOVED AND REPLACED PER AMM 53-11-02. LEAK CHECK ON TASK CARD [TTG8R008E5NT];[02] AFT CARGO DOOR FWD SCUFF PLATE; REPAIRED ON PO SDR SWAA2022092647075Scuff Plate · crackedAFT CARGO DOOR AFT SCUFF PLATE CRACKED AT STA 847 AFT CARGO DOOR AFT SCUFF PLATE P/N: 81205-146A8341-9 AT STA 847 CRACKED. / [01] REMOVED AND REPLACED PER AMM 53-11-02. LEAK CHECK ON TASK CARD [TTG8R008E5NT];[02] AFT CARGO DOOR AFT SCUFF PLATE ;REPAIRED ON PO SDR SWAA2022092647062None · looseLEFT AFT OVERWING EMERGENCY EXIT DOOR ESCAPE ROPE RETENTION STRAP; VELCRO IS NOT SECURED TO FUSELAGE. / [01] SECURED VELCRO PER AMM 20-10-06.;[02] INSPECTED WORK PERFORMED.SDR SWAA2022092647063None · looseRIGHT AFT OVERWING EMERGENCY EXIT DOOR ESCAPE ROPE RETENTION STRAP; VELCRO IS NOT SECURED TO FUSELAGE. / [01] SECURED VELCRO PER AMM 20-10-06.;[02] INSPECTED WORK PERFORMED.SDR SWAA2022092678496None · looseLEFT AFT OVERWING EMERGENCY EXIT DOOR ESCAPE ROPE RETENTION STRAP; VELCRO IS NOT SECURED TO FUSELAGE. / [01] SECURED VELCRO PER AMM 20-10-06.;[02] INSPECTED WORK PERFORMED.SDR SWAA2022092678497None · looseRIGHT AFT OVERWING EMERGENCY EXIT DOOR ESCAPE ROPE RETENTION STRAP; VELCRO IS NOT SECURED TO FUSELAGE. / [01] SECURED VELCRO PER AMM 20-10-06.;[02] INSPECTED WORK PERFORMED.SDR SWAA2022071828265Battery Pack · inoperativeFWD SERVICE DOOR EMERGENCY LIGHT INOP. / [01] REMOVED AND REPLACED FWD EMERGENCY LIGHTS BATTERY PACK PER AMM 33-51-06. LIGHTS OPS CHECK GOOD.SDR SWAA2021092320306Light · looseFLOOR EMERGENCY LIGHT STRIP ;OOSE AT ROW 12; FO SIDE / RESECURED EMER LIGHT STRIP AT ROW 12 IAW AMM 33-51-15SDR SWAA2021080299044Retainer · out of adjustFORWARD ENTRY DOOR LEFT GIRT BAR CLIP TIGHT / ADJUSTED GIRT BAR PER S.I.P.SDR SWAA2021031755255Slide · out of positionGIRT MATERIAL HANGING FROM GIRT PACK L2 DOOR / REPOSITIONED SLIDE GIRT PER MT 725-61-06 ACCOMPLISHED W.O. 763029SDR SWAA2021080316918Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140AF CORRODED / FOUND CORROSION LENGTH TO EXCEEDS MAX AMOUNT OF 20'. THIS IS OUT OF LIMITS. FABRICATED NEW AFT CARGO FLOOR PANEL 140AF IAW AMM 25-52-01-201; SRM 53-00-53-1A AND DRAWING PL 453A2610 REV KSDR SWAA2021081116360Strip · corrodedAFT CARGO BAY DOOR FORWARD CAP STRIP CORRODED / AFT CARGO BAY DOOR FWD CAP STRIP HAS NO SRM PUBLISHED LIMITS; OUT OF LIMITS.IAW SRM 53-00-53-1A-1 OBTAINED NEW CAP STRIP P/N 453A2611-1 A80459; REPLACED ON RACK I.A.W. IPC 25-52-10-04. CAP STRIP INSTALLED ON W/O SDR SWAA2021080316644Skin · damagedR/H WINGLET FASTENER HOLE OUT OF ROUND; UPPER SURFACE; 1 1/2' FWD OF T/E; 1/2' O/B OF WING MATING SURFACE / REPAIRED AREA AROUND FASTENER HOLE ON R/H WINGLET WITH NO DAMAGE TO FASTENER HOLE. IAW B737-800 SRM 57-31-00-200-801; APB AP37.8-0615; APB AP37.1-0632; SDR SWAA2021080316481Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140CF CORRODED / EVALUATED CORROSION ON AFT CARGO COMPARTMENT FLOOR PANEL 140CF CORROSION FOUND TO BE BEYOND 20 INCHES IN LENGTH OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW PANEL IAW AMM 25-52-01-201-801 TREATED AND PRISDR SWAA2021080316363Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140BF CORRODED / EVALUATED CORROSION ON FLOOR PNL AT AFT CARGO PNL 140BF FOUND CORROSION MORE THAN 10 INCHES FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW FLOOR PNL IAW SRM 51-40-05-0G-0 AND MM 25-52-01-201-801 AND SDR SWAA2021080316364Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140DF CORRODED / EVALUATED CORROSION AT AFT CARGO COMPARTMENT FLOOR PANEL 140DF TOTAL LENGTH EXCEEDS 20' MAXIMUM OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW PNL 140DF IAW AMM 25-52-01-201-801 AND BOEING DWG # 453A2610 RSDR SWAA2021080316362Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140EF CORRODED / AFT CARGO FLOOR PANEL 140EF CORRODED. 'OUT OF LIMITS' CORROSION IS PASSED 20' AND HAS MULTIPLE DAMAGE I/A/W SRM 53-00-53-1A-1 STEP 5A(B) FIG 102. FABRICATED NEW FLOOR PANEL 140EF I/A/W AMM 25-52-01-201-801 ALSSDR SWAA2020093016491Angle · crackedWING CENTER SECTION STA 663 LBL 10 REAR SPAR TO TANK ANGLE HAS CRACK AT FASTENER HOLE. ACCOMPLISHED A REPAIR ON UPPER REAR SPAR VAPOR BARRIER ATTACH ANGLE AT WING CENTER SECTION STA 663 LBL 7 TO LBL 23, IAW SRM 57-10-10-2R-5 STEP 4.SDR SWAA2020092916482Floor Panel · damagedCABIN FLOOR PANEL 242CF FWD INBOARD EDGE HAS DAMAGE. REPAIRED DAMAGED CORE AT FWD INBOARD EDGE OF PANEL 212CF, IAW B737-800 SRM 53-00-50-2R-10 SRM 53-0-50-2R-0.SDR SWAA2020092916483Floor Panel · damagedCABIN FLOOR PANEL 242AF AFT INBOARD EDGE HAS DAMAGE. REPAIRED AREA OF DAMAGED CORE AT AFT INBOARD EDGE OF PANEL 242AF, IAW B737-800 SRM 53-00-50-2R-10 SRM 53-00-50-2R-0.SDR SWAA2020092916484Floor Panel · damagedCABIN FLOOR PANEL 242BF FWD INBOARD EDGE HAS DAMAGE. REPAIRED AREA OF DAMAGED CORE AT FWD INBOARD EDGE OF PANEL 242BF, IAW B737-800 SRM 53-00-50-2R-10 SRM 53-00-50-2R-0.SDR SWAA2020092916490Angle · crackedWING CENTER SECTION STA 663 RBL 35 REAR SPAR TO TANK ANGLE HAS CRACK AT FASTENER HOLE/WING CENTER SECTION STA 663; RBL 35 REAR SPAR TO TANK ANGLE. CUT OUT AND REMOVED DAMAGE AND INSTALLED NEW REPAIR ANGLES, IAW SRM 57-10-10-2R-5 REPAIR 5 DWG. 111A1000 REV A. SDR SWAA2021082096177Support · crackedLEFT WING TRAILING EDGE UPPER FIXED PANEL SUPPORT IS CRACKED JUST INBOARD OF THE DEFLECTION CONTROL RIB / REMOVED CRACKED L/H WING TRAILING EDGE UPPER FIXED PANEL SUPPORT JUST I/B OF DEFLECTION CONTROL RIB AND INSTALLED NEW PANEL SUPPORT ALL IAW SRM 51-40-02-0SDR SWAA2021081716164Bracket · crackedRIGHT WING T/E PANEL 651FB FWD BRACKET IS CRACKED / REMOVED CRACKED FWD BRACKET FROM RIGHT WING T/E PANEL 651FB AND REPLACED WITH NEW FWD BRACKET P/N 287A9752-24 IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A2710 ATAG A80755SDR SWAA2021081116180Strip · damagedAFT CARGO COMPARTMENT FWD BULKHEAD PANEL 142NW CRUSHED/CRACKED ALONG WITH ASSOCIATED CAP STRIP / REMOVED AND REPLACED AFT CARGO PIT FWD BULKHEAD PANEL I/A/W MM 25-52-18 TAG# WN1209SDR SWAA2021080316191Floor Panel · corrodedFWD PIT FLOOR PANEL 120CF UPPER SURFACE EDGES CORRODED STA 500 TO 500C LBL24 TO RBL24 AT WL157 / EVALUATED CORROSION ON FWD PIT FLOOR PANEL 120CF UPPER SURFACE STA 500 TO 500C LBL 24 TO RBL 24 AT WL157; TOTAL CORROSION DAMAGE LENGTH EXCEEDS 20' MAXIMUM ALLOWEDSDR SWAA2021080316196Floor Panel · corrodedFWD PIT FLOOR PANEL 120AF UPPER SURFACE EDGES CORRODED STA 400 TO 440 RBL24 AT WL157 / EVALUATED CORROSION ON FWD PIT FLOOR PANEL 120AF UPPER SURFACE EDGES STA 400 TO 440 RBL 24 AT WL157 CORROSION DAMAGE FOUND TO BE OUT OF LIMITS DUE TO EXCEEDING 20' MAXIMUM ASDR SWAA2021080316194Floor Panel · corrodedFWD PIT FLOOR PANEL 120BF UPPER SURFACE EDGE CORRODED STA 500+8 LBL24 AT WL157 / VERIFIED LIMITS ON FWD CARGO FLOOR PANEL: LENGTH OF DAMAGE = 24' LIMIT = 20'. FWD CARGO FLOOR PANEL 120BF IS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102. FABRICATED NESDR SWAA2021080316187Floor Panel · corrodedFWD PIT FLOOR PANEL 120DF UPPER SURFACE EDGES CORRODED STA 500D TO 500I LBL24 TO RBL24 AT WL157 / FWD CARGO FLOOR PNL 120DF CORRODED ALONG UPPER EDGES CORROSION EXCEEDS ALLOWABLE DAMAGE 'OUT OF LIMITS' IAW 53-00-53-1A-1 FIG 102 FABRICATED NEW FLOOR PNL 120DF ISDR SWAA2021072116184Floorbeam · corrodedFWD PIT STA 500I LBL20 TO RBL24 LATERAL FLOOR SUPPORT UPR SURFACE CORRODED AT WL157 / REMOVED AND REPLACED BULKHEAD SUPPORT RAIL AT STA 500I IN FWD CARGO COMPARTMENT IAW SRM 51-40-02-0G-0 AND BOEING DWG# 143A7902 REV B WN4269SDR SWAA2021060816195Shield · corrodedAFT CARGO COMPARTMENT R/H FLOOR SHIELD BS847-867; WL157; RBL25 CORRODED / REMOVED CORROSION FROM AFT CARGO SHIELD AT BS 847-867 RBL 25 IAW SRM 51-10-02-0G-0. VERIFIED LIMITS; ORIGINAL THICKNESS .050'; LOSS OF .010'; REMAINING .040' OUT OF LIMITS IAW SRM 53-60-SDR SWAA2021060816190Shield · corrodedAFT CARGO COMPARTMENT R/H FLOOR SHIELD BS767-787; WL156; RBL24 CORRODED / AFT CARGO COMPARTMENT R/H FLOOR SHIELD BS 767-787 WL 156 RBL 24 CORRODED. REMOVED CORROSION AND 10X VISUAL INSPECTION IAW SRM 51-10-02-0G-0. VERIFIED LIMITS; FOUND TO BE OUT OF LIMITS IASDR SWAA2021060816178Shield · corrodedFWD PIT STA 495 RBL24 FLOOR SUPPORT SHIELD UPPER SURFACE CORRODED AT WL157 / REMOVED CORROSION FROM FWD CARGO FLOOR SHIELD IAW SRM 51-10-02-0G-0 PAR 15 AND INSPECTED W/ 10X MAG GLASS VERIFIED MATERIAL LOSS TO BE = .005' ORIGINAL T = .032' LIMIT = .003' FOUND TSDR SWAA2020093016182Floor Support · corrodedFWD PIT STA 500A TO 500I RBL 24 FLOOR SUPPORT Z ANGLE UPPER SURFACE CORRODED AT WL157. REMOVED AND EVALUATED CORROSION ON FWD CARGO RT Z ANGLE FROM STA 500A TO 500I, IAW B737 SRM 51-10-02-0G-0 & 53-00-53-1A-2. FOUND OUT OF LIMITS WITH .008' LOSS, ORIG .040' SDR SWAA2020093016200Floor Support · corrodedFWD PIT STA 500A TO 500I LEFT FLOOR SUPPORT Z ANGLE UPPER SURFACE CORRODED AT LBL 24 AND WL 157. REMOVED CORROSION ON LEFT SIDE Z CHANNEL. ORIGINAL THICKNESS .040', MAX ALLOWABLE REMOVAL IS .004'. FROM BS 500A TO 500B+10' REMOVED .003'. THIS IS WITHIN LIMISDR SWAA2020092916174Strap · missingAFT RIGHT HAND STOW BIN, MEGAPHONE IS MISSING SHOULDER STRAP. REPLACED AFT MEGAPHONE WITH SERVICEABLE UNIT IN AFT RIGHT HAND STOW BIN, IAW CUSTOMER TASK CARD 725-000-00-03 PGS 16-17 ITEM 2+3. ATAG A80775; A48929 WN2830.SDR SWAA2020092916168Strap · missingG-7 GALLEY, MEGA PHONE IS MISSING SHOULDER STRAP. REPLACED G-7 GALLEY MEGAPHONE WITH SERVICEABLE UNIT, IAW CUSTOMER TASK CARD 725-000-00-03 PG 4 ITEMS 2+3 ATAG 48929 WN2830 A80777.SDR SWAA2020092916197Doubler · corrodedFWD PIT FLOOR STRAP ATTACH DOUBLER AT Z ANGLE UPPER SURFACE CORRODED STA 500C+17 AT LBL 24 AND WL 157. FWD CARGO ATTACH Z-ANGLE DOUBLER SURFACE CORRODED STA 500C+17 WL 157. BLENDED AND REMOVED CORROSION, IAW SRM 53-00-53-1A-2 STEP 2D(1); (2); (3). MATERIAL SDR SWAA2021082616108Fairing · delaminated(REF DEFECT NO 0536143) RH WING TO BODY FAIRING 192AR HAS A DENT WITH DELAMINATION 11.5' FROM FWD EDGE AND 13' FROM LH EDGE. ACCOMPLISH REPAIR / REPAIRED RH WING TO BODY FAIRING 192AR DENT AND DELAMINATION IAW B737 SRM 53-40-70-2R-1 REPAIR PARA 4 AND B737 SRM SDR SWAA2020093015953Panel · looseLEFT WING DEFLECTION CONTROL RIB ATTACH FASTENERS TO THE UPPER FIXED TRAILING EDGE PANEL LOOSE AND CAUSING WEAR DAMAGE. ACCOMPLISHED REPAIR ON LT WING DEFLECTOR CONTROL RIB UPPER TAB AND BEAM, IAW SRM 57-51-02-2R-1 AND 4.SDR SWAA2020093019456Rib · looseLEFT WING DEFLECTION CONTROL RIB ATTACH FASTENERS TO THE UPPER FIXED TRAILING EDGE PANEL LOOSE AND CAUSING WEAR DAMAGE. ACCOMPLISHED REPAIR ON LT WING DEFLECTOR CONTROL RIB UPPER TAB AND BEAM, IAW SRM 57-51-02-2R-1 AND 4.SDR SWAA2020042743797Floor Panel · deformed***DELAY ONLY*** CABIN FLOOR PANEL REPLACEMENT DUE TO POPPING / REPLACED FLOOR PANELSDR SWAA2020042743800Floorboard · damagedREMOVED CENTER FLOOR BOARD FROM STATIONS 610 TO 706 / INSTALLED NEW FLOOR BOARD PER AMM 53-21-00SDR SWAA2021040643507Floor Panel · poppedFLOOR CENTER AISLE MAKES POPPING NOISE FROM ROW 15 TO 17.REPETITIVE INSPECTION ACTION: PERFORM GENERAL VISUAL EXAMINATION OF THE PANET TO ENSURE PANEL IS FREE OF DEFECTS (CRACKS;DENTS;PUNCTURES ETC) IF DEFECTS ARE NOTED CONTACT SERVICE ENGINEERING. INSPECTION SDR SWAA2022031250919Retainer · crackedLEFT WING AFT OF 31 PYLON UPPER FIXED TRAILING EDGE PANEL OUTBOARD UPPOR BRACKET CRACKED AT DEFECTION ROLLER BEAM ATTACH POINT / REMOVED AND REPLACED LH WING SUPPORT BRACKET AT DEFLECTOR ROLLER BEAM ATTACH POINT AFT OF #1 PYLON IAW SRM 51-40-02INSP 49017SDR SWAA2019012328825Light · brokenCENTER OVERHEAD EMERGENCY EXIT LIGHT BROKEN. R&R LIGHT ASSEMBLY IAW AMM.SDR SWAA2019010428218Lens · brokenOVERWING EXIT CEILING SIGN LENS BROKEN. R&R LENS PER MM.SDR SWAA2019010227889Sign · looseMID CABIN CEILING EXIT SIGN LOOSE. SECURED SIGN PER MM.
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