Boeing 737-7L9
Service difficulty reports · 1,024
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 = '7377L9' 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 = '7377L9' 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 SWAA2020060977743Cargo Track · corrodedCORROSION ON RAIL AT ACB BS 727D+6 RBL7 WL157. REPAIRED RAIL AT ACB BS 727D+6 RBL17 WL157 IAW SRM 53-00-53-2R-2 REPAIR 2.SDR SWAA2020060977705Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS400 LBL24 WL155. REMOVED AND REPLACED ANGLE AT INTERCOSTAL BS400 LBL24 WL155 PER REF SRM 51-40-02-0G AND DWG NR 143A7505.SDR SWAA2020060977721Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500B AFT SIDE LBL24 WL156. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BSS 500B AFT SIDE LBL 24 WL 156 PER REF SRM 51-40-02-0G AND DWG NR 143A7502; 143A7505.SDR SWAA2020060977720Support Angle · corrodedCORROSION ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FCB BS500D LBL29 WL158. REMOVED AND REPLACED SIDEWALL SUPPORT ANGLE AT AFT BULKHEAD FCB BS500D LBL29 WL158 PER REF SRM 51-40-02-0G AND DWG NR 143A9481.SDR SWAA2020060977719Support Angle · corrodedCORROSION ON AFT BULKHEAD TO FLOOR PANEL SUPPORT ANGLE AT FCB BS500D LBL22 TO RBL23 WL157. REMOVED AND REPLACED AFT BULKHEAD TO FLOOR PANEL SUPPORT ANGLE AT FCB BS500D LBL22 TO RBL23 WL157 PER REF SRM 51-40-02-0G AND DWG NR 143A9481.SDR SWAA2020060877733Splice · corrodedCORROSION ON FLOOR SUPPORT SPLICE AT ACB BS767+6 LBL19 - RBL19 WL157. CORROSION ON FLOOR SUPPORT SPLICE AT ACB BS767+6 LBL19-RBL19 WL157 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. DENT IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PAR 9C. REMOVSDR SWAA2020051176157Battery Pack · dischargedAFT EMERG. BATTERY PACK INOP / R/R AFT EMERGENCY BATTERY PACK IAW AMM 33-51-06. OPS CK. GOOD.SDR SWAA2021071476538Floorbeam · crackedPANEL BREAK SUPPORT AT BS 540; BL 0- RBL 25 IS CRACKED. / REMOVED & REPLACED PANEL BRAKE SUPPORT-36 PER SRM 51-40-02-0G-0 & AIPC 53-31-00-05 PG 31 59899U 13MAY20SDR SWAA2021051276530Skate Angle · chafedLT AFT VERTICAL FIN TO BODY SKATE ANGLE HAS CHAFFING DAMAGE AT BS 1025 AND BS 1132. REMOVED AND REPLACED LH AFT VERTICAL FIN TO BODY SKATE ANGLE AT BS1016 BS 1132 IAW SRM 514002 DWG 148A8300 AND DWG 148A3590.SDR SWAA2021051276531Skate Angle · chafedRT AFT VERTICAL FIN TO BODY SKATE ANGLE HAS CHAFFING DAMAGE AT SEVERAL AREAS FROM BS 1025- BS 1132. REMOVED AND REPLACED RH AFT VERTICAL FIN TO BODY SKATE ANGLE AT BS 1016 BS 1132 IAW SRM 514002 DWG 148A8300 AND DWG 148A3590SDR SWAA2021051276529Skate Angle · chafedLT FWD VERTICAL FIN TO BODY SKATE ANGLE HAS CHAFFING DAMAGE AT BS 1016. REMOVED AND REPLACED LT FWD SKATE ANGLE AT BS 1016 IAW SRM 514002; DWG 147A0030 AND DWG 147A0070. APPLIED DECORATIVE EXTERIOR; PAINT IAW AMM 512199300801SDR SWAA2020060976532Stiffener · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 120.30 2ND VERTICAL STIFFENER IS CRACKED. REPAIRED RT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-5.SDR SWAA2020060976533Stiffener · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 120.30 3RD VERTICAL STIFFENER IS CRACKED. REPAIRED RT HORIZONTAL STABILIZER INSPAR RIB STAB STA 120.30 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-5.SDR SWAA2020060976534Stiffener · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 120.30 4TH VERTICAL STIFFENER IS CRACKED. REPAIRED RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 4TH VERTICAL STIFFENER IAW SRM 55-10-09-2R-5.SDR SWAA2020060976535Stiffener · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 120.30 3RD VERTICAL STIFFENER IS CRACKED. REPAIRED LT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 3RD VERIFIED STIFFENER IAW SRM 55-10-09-2R-5.SDR SWAA2021081676527Skin · crackedCRACK AROUND THE FASTENER AT RIGHT WING NO.8 SLAT LOWER SURFACE NOSE SKIN AT ACTUATOR RIBS. / REMOVED; INSTALLED SERVICEABLE; ADJUSTED AND FUNCTIONAL TESTED #8 SLAT IAW MM 27-81-21-000-801 AND MM 27-81-21-000-801 AND MM 27-81-21-400-801 FUNCTIONAL CHECK GOOD VSDR SWAA2021072676526Skin · crackedCRACK AROUND THE FASTENER AT LEFT WING NO.1 SLAT LOWER SURFACE NOSE SKIN AT ACTUATOR RIBS. / REMOVED AND REINSTALLED SERVICEABLE #1 SLAT PER MM 27-81-21-400-801 ADJUSTED AND FUNCTINALLY TEST PER MM27-81-00-820-803 OPS CHECK GOOD VERIFIED ALL TORQUES SAFTIES ANSDR SWAA2020060976528Skin · crackedCRACK AROUND THE FASTENER AT RIGHT WING NR 6 SLAT LOWER SURFACE NOSE SKIN AT ACTUATOR RIBS. TRIMMED OUT THE DAMAGE PART OF RIGHT WING NR 6 SLAT LOWER SURFACE NOSE SKIN AT ACTUATOR RIB AND INSTALLED REPAIR PARTS IAW SRM 57-42-01-2R-8.SDR SWAA2020050674688Battery · dischargedLEFT & RIGHT OVER WING EMERGENCY LIGHTS INOP / REMOVED & REPLACED R/H & L/H EMERGENCY SIGN BATTERY AT STA @40 REF AMM 33-51-06SDR SWAA2020040735940Slide · looseR2 DOOR SLIDE LOOSE / SECURED R2 DOOR SLIDE REF MT 725-61-06; AMM 25-66-01SDR SWAA2020030942307Slide · out of position"Z" FOLD HAS COME OUT OF CONTAINER AT LH AFT SLIDE GIRT REPOSTIONED L2 SLIDE THAT IS HOOKED TO THE GERT BAR REF MM 25-66-01 (DID NOT REMOVE SLIDE FROM COVER) REF SA-M 767 H24793-3SDR SWAA2021081712418Splice Strap · corrodedAFT CARGO COMPARTMENT. STA 727D+4; RBL 21 TO LBL 21; WL 155; FLOOR PANEL SPLICE STRAP HAS CORROSION ON UPPER AND LOWER SURFACE. / REPLACED NEW TEE ASSY ON AFT CARGO COMPARTMENT; STA 727D+4 RBL 21-LBL 21; WL 155; IAW BOEING DWG #146A7500 TY: DWG; ID: 0037 REV: SDR SWAA2021062912415Scuff Plate · crackedAFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED / WELDED AFT CARGO DOOR AFT CORNER SCUFF PLATE IAW SHOP WORK REQUEST 40430/1600/003SDR SWAA2020022094568Plate · crackedR/H WING FIXED TRAILING EDGE OUTBOARD OF #6 FLAP TRACK HAD CRACKED WAFFLE PLATE. / R&R WAFFLE PLATE IAW SRM AND DWG.SDR SWAA2020022041608Crease Beam · corrodedR2 DOOR CREASE BEAM CORRODED BETWEEN BS. 927 TO BS. 967. / R&R R2 DOOR CREASE BEAM IAW SRM AND DWG.SDR SWAA2021041312405Angle · corrodedAFT PIT RH Z ANGLE HAS MULTIPLE AREAS OF CORROSION BETWEEN STA 747 TO STA 767. EVALUATED CORROSION ON AFT CARGO RH Z ANGLE FROM STA 747 TO STA 767; WL 160 AND RBL 20. FOUND TO BE OUT OF LIMITS DUE TO CORROSION ON FASTENER HOLES IAW SRM 5300531A2 FIG 103 SHEET SDR SWAA2020022871767Skin · incorrectSKIN INTERNAL BETWEEN BS. 611 TO BS. 615, BETWEEN STR. 1 TO STR. 2R REQUIRED REPLACEMENT. / R&R FUSELAGE SKIN IAW EA.SDR SWAA2021082512402Pan · corrodedAFT WET AREA; STA 1016 + 6'; LBL 15; WL 208; LAV PAN CORRODED AT FASTENER HOLE. / EVALUATED CORROSION ON LAV PAN IN AFT WET AREA AT STA 1016+6'; LBL 15 AND WL 208. FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA IAW SRM 51-10-02-0G-0 STEP 9. REMOVED AND REPSDR SWAA2020022094567Strap · corrodedAFT WET AREA FLOOR STRUCTURE STRAP CORRODED AT BS. 1016+11, BL 0. / R&R STRAP PER SRM AND DWG.SDR SWAA2020021241316Slide · dislodgedL1 DOOR SLIDE PARTIALLY FELL OUT OF CASE. / R&R SLIDE IAW MT.SDR SWAA2021082322395Floor Panel · corrodedAFT CARGO COMPARTMENT PANEL 140BF HAS CORROSION AROUND THE EDGES / AFT CARGO COMP PANEL 140BF CORROSION FOUND TO BE 'OUT OF LIMITS' WITH MAX LENGTH OF 20' EXCEEDED IAW SRM 53-00-53-1A-1 FABRICATED NEW PANEL IAW BOEING DWG #453A2610 REV. K AND SRM 51-40-05-0G-0SDR SWAA2021081712396Floor Panel · corrodedAFT CARGO COMPARTMENT PANEL 140DF HAS CORROSION AROUND THE EDGES / CORROSION DAMAGE ON PNL 140DF EXCEEDS 20'; OUT OF LIMITS; FABRICATED NEW PNL 140DF; P/N 453A2610-20; ACCOMPLISHED CONFROMITY INSPECTION AND VERIFIED FLOOR PANEL P/N 453A2610-20 CONFORMS TO THE SDR SWAA2021081712394Floor Panel · corrodedAFT CARGO COMPARTMENT PANEL 140AF HAS CORROSION AROUND THE EDGES / CORROSION DAMAGE EXCEEDS 20'; OUT OF LIMITS; FABRICATED NEW PNL 140AF P/N 453A2610-34; ACCOMPLISHED CONFORMITY INSPECTION AND VERIFIED FLOOR PANEL P/N 453A2610-34 CONFORMS TO THE SPECIFICATIONSSDR SWAA2021082322381Frame Splice · corrodedAREA AFT OF AFT CARGO PIT; STA967; RBL18; WL183 FRAME SPLICE PLATE; JUST FWD OF OUTFLOW VALVE CUTOUT; HAS CORROSION ON UPPER LIP OF PLATE. / REMOVED CORROSION AT AFT CARGO STA 967 RBL 18 WL 183 FRAME SPLICE PLATE IAW SRM 53-00-04-1A-1. VERIFIED MATERIAL LOSS OSDR SWAA2021041312379Angle · corrodedAFT CARGO PIT LH Z ANGLE STA 767+3' TO STA 847; WL 158 HAS MULTIPLE AREAS OF CORROSION REMOVED CORROSION FROM AFT CARGO LH Z ANGLE STA 767+3 TO 847 IAW B737 SRM 5110020G0 FOUND TO BE OUT OF LIMITS ORIG .040 REMAIN .020' LOSS .020' IAW B737 SRM 53005312. ZANGLESDR SWAA2021040212377Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 241AAF UPPER SURFACE HAS FIBER DAMAGE / REPAIRED UPPER SURFACE PLY ON FLOORBOARD 241AAF IAW SRM 53-00-50-2R-1; PG'S 1;2 STEPS 3(A-N) A05073;A10203SDR SWAA2021040212375Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 242VF UPPER SURFACE HAS FIBER DAMAGE / WORK PERFORMED ON WORK CARD # 40428/2700/0019SDR SWAA2021040212373Floor Panel · damagedPASSENGER CABIN AFT WET AREA FLOOR PANEL 242XF HAS FIBER AND CORE DAMAGE / REPLACED PNL242XF IAW 53-00-50-2R-1 REV 69 51-00-05 NDT EVALUATED AND FOUND FIBER DAMAGE AND CORE DAMAGE REPAIRED IAW B737 SRM 53-00-50-2R-0 REV 69 (A89485)(A98054)SDR SWAA2020022041607Angle · corrodedAFT CARGO PIT L/H Z ANGLE HAD MULTIPLE AREAS CORRODED BETWEEN BS. 727+3 TO BS. 847, WL 158. / R&R Z ANGLE IAW SRM AND DWG.SDR SWAA2021040212348Floor Panel · dentedDOT #008; CABIN FLOOR PANEL 241BF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED 5 AREAS WITH DENT DAMAGE AT UPPER FACESHEET ONLY ON FLOORBOARD 241BF IAW B737 SRM 53-00-50-2R-1; PAR 3(A; C; E; K1; L1; M1) -REV 69 & SRM 53-00-50-2R-0; PAR (5)- REV 69.SDR SWAA2021040212359Floor Panel · dentedDOT #015; CABIN FLOOR PANEL 241EF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED CABIN FLOOR PANEL #241EF OF 1(EA) DENT IAW B737-700 SRM 53-00-50-2R-0 REV 69 AND B737-700 SRM 53-00-50-2R-4 REV 69 AND 2(EA) DENTS IAW B737-700 SRM 53-00-50-1A-1 REV 69. A89485; A36SDR SWAA2021040212357Floor Panel · dentedDOT #013; CABIN FLOOR PANEL 242DF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED PNL 242DF SEVERAL DENTS ON UPPER SURFACE. IAW B737-700 SRM 53-00-50-2R-1 REV 64; SRM 53-00-50-2R-0 REV 69 A98054; A36551SDR SWAA2021040212355Floor Panel · dentedDOT #012; CABIN FLOOR PANEL 242BF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED CABIN FLOOR PANEL 242BF PUNCTURE 2' AFT OF FWD EDGE AND 2 1/2' O/B FROM I/B EDGE IAW B737 SRM 53-00-50-2R-1 REV 69 AND B737 SRM 53-00-50-2R-0 REV 69; AND MULTIPLE DENTS ON UPPER SURSDR SWAA2021040212353Floor Panel · dentedDOT #010; CABIN FLOOR PANEL 242AF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED UPPER SURFACE PLY ON FLOORBOARD 242AF IAW SRM 53-00-50-2R-1; PG'S 1;2; & FOUND DENTS 3EA TO BE WITHIN LIMITS IAW SRM 53-00-1A-1; PG 2; ITEMS C (1;2;3) A05073; A10203SDR SWAA2021040212347Floor Panel · dentedDOT #007; CABIN FLOOR PANEL 232RF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED DENTS THAT WERE OUT OF LIMITS IAW SRM 53-00-50-2R-2 ITEM 3 (A THROUGH M ) ON PASSENGER CABIN FLOORBOARD 232 RF; UPPER SURFACESDR SWAA2021040212331Floor Panel · dentedDOT #003; CABIN FLOOR PANEL 231ZF HAS SEVERAL DENTS; UPPER SURFACE. / DENTS REPAIRE DON UPPER FLOOR BOARDS SURFACE ON FLOOR BOARD 231 ZF. IAW SRM 53-00-50-2R-2 ITEM 3 STEPS A THROUGH NSDR SWAA2021040212339Floor Panel · dentedDOT #004; CABIN FLOOR PANEL 231YF HAS SEVERAL DENTS; UPPER SURFACE. / REPAIRED DAMAGE ON FLOOR PANEL 231YF. BLENDED REPIAR PLIES IN 3EA LOCATIONS. CURED; TAP TEST GOOD. IAW B737-700 SRM 53-00-50-2R-0 REV 69; SRM 53-00-50-2R-1 REV 69SDR SWAA2021072012323Stiffener · crackedFOUND DURING FCBS REPAIR SURVEY MLG WHEEL WELL CENTER WING REAR SPAR STA 663 RBL 27 APPROXIMATE WL 153 VERTICAL STIFFENER IS CRACKED 2.5 INCHES LONG / REMOVED DAMAGED STIFFENER IN MLG WHEEL WELL @ STA 663 RBL 27 WL 153' AND INSTALLED NEW STIFFNER P/N 11A 308-1SDR SWAA2021072012255Handle · crackedDURING INSPECTION OF THE REPAIR SURVEY FOR THE FWD CARGO DOOR; FOUND DOOR HANDLE CRACKED ON THE INSIDE AROUND RIVET BUCKTAIL (MARKED) / REMOVED CRACKED FWD CARGO DOOR HANDLE PAN AND INSTALLED NEW HANDLE PART IAW EA 200170 REV P1; IR & SWA EA 1-752-2698 REV IR SDR SWAA2022032503666Bracket · crackedLEFT HAND WHEEL WELL AT FROUNT SPAR BRACKET TO UPPER SHELF PANEL IS CRACKED / REMOVED AND REPLACED FRONT SPAR BRACKET PER SRM. 51-40-02
Back to Boeing 737-7L9