Boeing 737-7CT
Service difficulty reports · 2,415
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 = '7377CT' 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 = '7377CT' 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 SWAA2021062173413Channel · missingAFT CARGO COMPARTMENT FLOOR SUPPORT 'Z' CHANNEL TO FRAME MISSING 1/4' ATTACH BOLT B.S. 727+5 R.BL. 21'(51-001) ; / INSTALLED BOLT AT STA. 727 PLUS 5 RBL 21 ON FLOOR SUPPORT Z CHANNEL PER REF. B 737 SRM 51-40-02-0G AND DRAWING # 146A0061; VERIFIEDSDR SWAA2021062173412Channel · corrodedCORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT 'Z' CHANNEL AT NUT PLATE HOLES B.S. 727C - 767 R.BL. 22'.(51-002) ; / APPLIED TOP COAT PER B 737 AMM51-21-73-370-804;INSTALLED NUT PLATES PER REF DRAWING 146A7500 AND B737 SRM 51-40-02-0G-0 ON FABRICATED Z CHANNSDR SWAA2021062172992Channel · crackedFWD CARGO COMPARTMENT FLOOR STRUCTURE ZEE CHANNEL CLIP AT RBL21.00 AND STA 400 CRACKED ; / OK TO TREAT AND PRIME NEW HOLE'S;INSTALLED NEW CLIP AS PER B737-700 ARM 51-40-02-0G-0;LOCATED AND DRILLED NEW CLIP AS PER B737-700 ARM 51-40-05-0G-0;REMOVED AND REPLACEDSDR SWAA2021051772994Channel · corrodedFWD CARGO FLOOR STRUCTURE ZEE CHANNEL UPPER SURFACE AT RBL21.00 AND ABOUT STA 500+15 WITH CORROSION ; /SDR SWAA2021051772993Angle · crackedFWD CARGO COMPARTMENT FLOOR STRUCTURE ZEE CHANNEL CLIP AT LBL21.00 AND STA 400 CRACKED ; /SDR SWAA2021062171587Seat Track · corroded**CORROSION** CABIN SEAT TRACK STA 520 AT LBL 45.50 UPPER CROWN WITH CORROSION ; / CUT OUT SEAT TRACK AT LBL 45.50 STA 491-521 REF SRM 53-00-52-2R-4 STEP 4B;INSPECTED SEAT TRACK INSTALLATION;INSPECTED LOCATED AND DRILL SPLICE;INSTALLED FLOOR PANELS 231VF AND 2SDR SWAA2021062171594Attach Angle · crackedCUSTOMER REQUEST--RH WHEEL WELL VAPOR BARRIER STA.663 TOP ATTACH ANGLE CRACKER TWO PLACES RBL12 AND RBL48 ; / ACCOMPLISHED REPLACEMENT VAPOR BARRIER WEB UPPER ANGLE AT STA 663 RBL-6 TO RBL-60 REF B737-700 SRM 51-40-02-0G-0;CAP SEALING VERTICAL AND HORIZONTAL LSDR SWAA2021061871588Seat Track · corrodedCORROSION CABIN SEAT TRACK STA 520 AT LBL 24.75 UPPER CROWN WITH CORROSION ; / ACCOMPLISHED SEAT TRACK INSTALLATION AT MAIN CABIN FROM STA 490-521 LBL-24.75 REF B 737-700 SRM 53-00-52-2R-4;CUT OUT SEAT TRACK AT LBL 24.75 STA 490-521 REF B373-700 SRM 53-00-52-2SDR SWAA2021051771574Seat Track · corroded**CORROSION** CABIN SEAT TRACK BETWEEN STA 727E AND 747 AT RBL 45.50 LOWER CROWN WITH CORROSION ; /SDR SWAA2021051771573Seat Track · corrodedCORROSION CABIN SEAT TRACK AT STA 727C LBL 45.50 LOWER CROWN WITH CORROSION ; /SDR SWAA2021062171137Floor Support · crackedINTERCOSTAL WITH A CRACK ON UPPER SURFACE AT CABIN FLOOR STRUCTURE AT ABOUT BL-0 BETWEEN STA 344-360 ; / INSTALLED EWIS PROTECTION;LOCATED AND DRILL NEW INTERCOSTAL BETWEEN FS 344-360 BL 0;OK TO TREAT AND PRIME AREA;OK TO INSTALL INTERCOSTAL;REMOVED INTERCOSTASDR SWAA2021062171136Floor Panel · deterioratedAFT CARGO COMPARTMENT FLOOR PANEL #140BF WORN/DETERIORATED. ; / FABRICATED AFT CARGO FLOOR PANEL 140 BF PER REF B737 AMM 25-52-01-201-801 USING REMOVED PANEL AS TEMPLATE MAT. USED .071 2024 T3 CLAD;FABRICATED FLOOR PANEL 140 BF PER REF B737 AMM 25-52-01-201-80SDR SWAA2021062171132Spar · crackedRT HORIZONTAL UPPER REAR SPAR TRACK ASSY IS CRACKED AT UPPER END. ; / ADDING PART INSTALL INFORMATION.;ADDING PARTS REMOVAL TO ITEM;INSTALLED R\H HORIZONTAL UPPER REAR SPAR TRACK ASSY PER B737 SRM 51-40-02-0G-0.;OK TO INSTALL NEW UPPER SPAR TRACK.;REMOVED R\H SDR SWAA2021051771557Scuff Plate · corrodedCABIN PAX L1 DOOR BET STA312 TO STA344 CUTOUT THRESHOLD SCUFF PLATE AREA SIDE PLATE O/B ANGLE; SURFACE CORROSION ; /SDR SWAA2021062170544Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 231YF UPPER SURFACE AFT END DELAMINATED. (18-026) ; / NO INSPECTION;REPAIRED DAMAGE AREA ON AFT END OF MAIN CABIN FLOOR PANEL 231YF UPPER SURFACE AS PER B737 SRM 53-00-50-2R-4 MATERIAL USED PO#1480720 AND PO# 1692653;REQUEST OK TO INSTSDR SWAA2021062170542Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 231ZF UPPER SKIN SURFACE AFT END DELAMINATED. (18-025) ; / CLEAN DAMAGE AREAS FOR REPAIR AS PER ARM <BR><BR>CLEAN DAMAGE AREA FOR REPAIR AS PER SRM 53-00-50-2R-4<BR> PARAG 3E;INSPECTED REPAIR AREA;MEASUREMENTS;OK TO REPAIR AREA;OK TO RSDR SWAA2021062170538Floor Panel · crackedCENTER CABIN FLOOR PANEL 232SF UPPER SKIN SURFACE CRACKED. (18-028) ; / CLEANED AND PREPARED PANEL #232SF FOR REPAIR;LATE ENTRY OK TO INSTALL REPAIR UNDER RII;MEASUREMENTS;OK TO INSTALL REPAIR AT DAMAGE AREA;OK TO REPAIR PANEL #232SF;VERIFIED ALL SIGNOFFS;VERISDR SWAA2021062170533Floor Panel · peelingCENTER CABIN FLOOR PANEL 241BF UPPER SKIN SURFACE PEELING. (18-024) ; / CLEANED AND PREPARED DAMAGE AREAS FOR REPAIR ON TOP SURFACE OF FLOOR PANEL 241BF;MEASUREMENTS;OK TO INSTALL REPAIR;REPAIRED DAMAGE AS MARKED ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 241BF SDR SWAA2021062170531Connector · missingPAX SIDEWALL PANEL 232YHW HAS A MISSING CONNECTOR ON EMERGENCY LIGHT. ; / INSTALLED EMERGENCY LIGHT CONNECTOR AT SIDEWALL PANEL #232YHW AS PER REF B737 AMM33-51-01SDR SWAA2021062170529Floor Panel · peelingCENTER CABIN FLOOR PANEL 241FF UPPER SKIN SURFACE FWD AND AFT CORNERS HAS MATERIAL PEELING. (18-021) ; / INSPECTED REPAIRED PANEL FOUND SERVICEABLE.;MEASUREMENTS;ACCOMPLISH REPAIR AS PER B737 SRM 53-00-50-2R-4;CLEAN DAMAGE AREAS 2EA. ON CORNERS OF MAIN CABIN FSDR SWAA2021050367277Girt Bar · out of adjustFWD SERVICE DOOR SLIDE ATTACHMENT/GIRT BAR IN LOW ; / REATTACHED/ADJUSTED VELCRO ATTACHMENTS ON SLIDE/GIRT BAR PER SIPSDR SWAA2021040560129Girt Bar · out of adjustFWD SERVICE DOOR SLIDE GIRT NEEDS ADJUSTMENT AND CLIP TIGHTED ADJUSTED SLIDE GIRT AND TIGHTENED CLIP ON FWD SERVICE PER AMM256601SDR SWAA2021030853350Light · brokenEMERGENCY LIGHT LENSE AND BEZEL BROKEN AT 16 D-E-F / OK TO CONTINUE PER MEL 25-10-01 SP1B TRACKING #70711SDR SWAA2021030853421Seat Track · failedFIRST OFFICERS I/B AFT SEAT TRACK FAILED CHECK / R&R FO'S I/B AFT SEAT TRACK PER M/M 25-11-11SDR SWAA2021030853420Seat Track · crackedCAPTAINS I/B AFT SEAT TRACK FAILED CHECK / R&R CAPTAINS I/B AFT SEAT TRACK PER M/M 25-11-11SDR SWAA2021030853418Girt Bar · out of adjustR1 DOOR SLIDE GIRT NEEDS REINSTALLED; TOO LONG. REINSTALLED R1 DOOR SLIDE GIRT PER AMM.256601 AND MT 7256106.SDR SWAA2021022450490Sign · missingFWD SERVICE DOOR EXIT SIGN NOT INSTALLED / R/R RIGHT ASSY PER AMM 33-51-01SDR SWAA2021021548724Door · out of adjustR1 DOOR RIDES HARD ON AFT UPPER LATCH RECEIVER WHEN CLOSING / PERFORMED R1 DOOR ADJUSTMENT PER B737 AMM 52-41-00-820-801 ALL OPS NORMAL PERFORMED PRESSURIZATIONAL LEAK TEST OF R1 DOOR REF B737 AMM 25-51-91-790-801; NO LEAKS FOUNDSDR SWAA2021021548485Skirt · out of adjustQA WALK*** R2 DOOR ESCAPE SLIDE SKIRT RUB SCUFF PLATE WHEN CLOSING. / ADJUSTED R2 DOOR SLIDE SKIRT RUB AS PER TASK CARD 8725-61-06SDR SWAA2021021848597Skin · crackedCRACK SLAT 3 CENTER FLEX SKIN LOWER SURFACE AT LT WING (1 EA) / REPAIRED CENTER FLEX SKIN LOWER SURFACE SLAT 3 AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10 AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL.TOOL USED CALIPER P/N:700-113-10; S/N: 0013226; DUSDR SWAA2021021748896Skin · crackedCRACK FIXED LEADING EDGE SKIN AT KRAS 185 AT RT WING. PERFORMED PERMANENT REPAIR ON FIXED LEADING EDGE SKIN AT KRAS 185 AT RT WING IAW EA 21-157-00362 REV IR AND EA 57-0046-21 REV 0 PART 1 MATERIAL USED FOR REPAIR PARTS:-1 FILLER AND -3 FILLER FROM 2024T3 0.0SDR SWAA2021021748895Skin · crackedCRACK FIXED LEADING EDGE SKIN AT KRAS 186 AT LT WING. PERFORMED PERMANENT REPAIR ON FIXED LEADING EDGE SKIN AT KRAS 186 AT LT WING IAW EA 21-157-00361 REV IR AND EA 57-0046-21 REV 0 PART 1 MATERIAL USED FOR REPAIR PARTS:-1 FILLER AND -3 FILLER FROM 2024T3 0.0SDR SWAA2021021747631Rib · crackedCRACK INSPAR RIB 120.30 ON LOWER CHORD AT 17.5 INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER. PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 LOWER CHORD AT 17.5 INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09- 2R-5 REPAIR 5 FIGURE 2SDR SWAA2021021646754Angle · crackedVERT STAB HAS ANGLE CRACKED ABOVE AND ON AFT SIDE OF FWD LEFT ATTACH LUG. / REMOVED AND REPLACED VERTICAL STAB LWR ANGLE ON FWD SIDE OF ATTACH LUG REF B737-700 SRM 51-40-02-0G-0 AND DWG #176A3101SDR SWAA2021021846497Reveal · crackedCRACK SERVICE DOOR CUT OUT REVEAL AT BS 294.5 BTW STR 14R TO STR 15R AT FWD GALLEY AREA. REPLACED REVEAL SERVICE DOOR CUT OUT AT BS 294.5 BTW STR 14R TO STR 15R AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 141A8370 REV; C PN USED:141A8372U2SDR SWAA2021041945681Bulkhead · damagedAFT CARGO COMPARTMENT; SHROUD 142NWA FOUND DAMAGED DURING INSPECTION. / RECEIVED NEW SHROUD 142NWA FROM STOCK .INSTALLATION WILL BE COMPLETED CUSTOMER CARD # JPANEL-141-CLOSE .SDR SWAA2021021546653Floor Panel · delaminatedCABIN PANEL 241 RF IS DELAMINATED AT AFT RIGHT HAND CORNER. / ACCOMPLISHED PERMANENT REPAIR AT CABIN FLOOR PANEL 241RF AFT RIGHT HAND CORNER PER REF B737 SRM 53-00-50-2R-9SDR SWAA2021021847104Light · brokenBROKEN ENTRY LIGHT PANEL HOUSING EXIT AT AFT GALLEY AREA. REPLACED ENTRY LIGHT PANEL HOUSING EXIT AT AFT GALLEY AREA IAW B737-700 AMM 33-511-01-960-802.SDR SWAA2021021644734Skin · corrodedCORROSION***ON LWR SURFACE OF LWR CTR WING SKIN AROUND 2 FWD BOLTS LBL 56 BS 541. / ACCOMPLISHED REPAIR OF CORROSION FOUND ON LWR SURFACE OF WING SKIN AROUND 2 FWD BOLTS LBL 56 BS 541 PER INSTRUCTIONS ON AAR RES-WI 2016690-11 REV IR AND SOUTHWEST EA 21-157-002SDR SWAA2021021848201Mount · deterioratedDETERIORATED ENTRY FWD DOOR CUT OUT MOUNT AT FWD GALLEY AREA (2 EA). REPLACED SHOCK MOUNT LOC ENTRY FWD DOOR CUT OUT AT FWD GALLEY AREA (2EA) DUE TO DETERIORATED NOT FOUND ALLOWABLE DAMAGE PART NUMBER USED BAC514K1 PO 202019825900101 IAW B737-700 SRM 51-40-02SDR SWAA2021021748067Skin · deterioratedDETERIORATED SERVICE DOOR CUT OUT MOUNT AT FWD GALLEY AREA (2 EA). REPLACED MOUNT LOCATED AT SERVICE DOOR CUT OUT AT FWD GALLEY AREA (2 EA) IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.SDR SWAA2021021544411Support · crackedFWD CARGO COMPARTMENT;GUSSET SUPPORT IS CRACKED AT STA 500D S-19LH. / REMOVED AND REPLACED GUSSET SUPPORT AT FWD CARGO COMP. AT STA 500D S-19LH AND TREATED ASS FASTENERS HOLES WITH ALODINE AND PRIME IN REF B737-700 SRM 51-40-02-0G-0; 51-20-01-0G-0 AND DWG# 143SDR SWAA2021021844905Screw · damagedDAMAGE SCREW ACCESS PANEL 343CB; 343DB; 333CB AND 333DB AT RT HORIZONTAL STABILIZER. REPLACED SCREWS ON ACCESS PANELS 343CB; 343DB; 333CB AND 333DB AT RIGHT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02.SDR SWAA2021070744995Seat Track · crackedCOCKPIT; CAPTIANS RACEWAYFOUND CRACKED. / REMOVED AND REPLACED COCKPIT; CAPTAINS RACEWAY WITH NEW RACEWAY AS PER REF B737-7 SRM 51-40-02-0G-0SDR SWAA2021021844903Structure · crackedCRACK INNER CHORD LOC ON FWD SERVICE DOOR BS 294.5 AT LEVEL STR 17R AND RBL52 AT FWD GALLEY AREA / REPLACED INNER CHORD LOCATED ON FWD SERVICE DOOR BS294.5 AT LEVEL STR17R AND RBL 52 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8310 SHEET 25 RSDR SWAA2021021544220Bracket · crackedFWD CARGO COMPARTMENT HAS CRACKED BRACKET AFT SIDE OF FRAME BS 500C S-26L. / REMOVED AND REPLACED BRACKET AT FWD CARGO COMP AT BS 500C; S-26L AND TREATED ALL FASTNERS HOLES WITH ALODINE AND PRIMER IN REF BB 737-700 SRM 51-40-02-0G-0; 51-20-01-0G-0 AND DWG # 14SDR SWAA2021021844902Reveal · crackedCRACK ON REVEAL LOC BS 294.5 BTW STR8R TO STR 9R FWD GALLEY AREA AT UPPER FUSELAGE / REPLACED REVEAL LOC. BS 294.5 BTW STR 8R TO STR 9R FWD GALLEY AREA AT UPPER FUSELAGE I.A.W SRM B737-700 51-10-02 ITEM 9 AND DRAWING 141A8370 REV:C REVEAL P/N USED:141A8372U1SDR SWAA2021071442583Bushing · out of toleranceFUSELAGE BULKHEAD FITTING LUG BS 1016 FOR VERTICAL STAB FRONT RIGHT ATTACHMENT HAS BUSHING OUT OF LIMITS. [0.8840'] [MAX ALLOWED 0.8835' TASK 55-30-00-200-801] / REMOVED AND REPLACED BUSHING AT FUSELAGE BULKHEAD FITTING LUG BS 1016 FOR VERTICAL STAB FRONT RIGHSDR SWAA2021021844883Ceiling Panel · crackedCRACK CEILING PANEL 120YAC (SHROUD PANEL) FWD CARGO COMPARTMENT.SDR SWAA2021021642585Rib · crackedRT WING UPPER T/E PNL AFT OF PYLON HAS CTR AFT RIB CRACKED AT FWD LWR BOLT HOLE. / REMOVED AND REPLACED CENTER AFT RIB AT RT. WING AFT OF PYLON IAW SRM 51-40-02-0G-0
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