N938WN
Service difficulty reports · 203
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 = 'N938WN' 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 = 'N938WN' 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 SWAA2021062374791Floor Panel · damagedFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS. / FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-6. 59702U 05/15/21SDR SWAA2021062370845Floor Panel · damagedFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS. / DUE TO EXTENT OF DAMAGE; REPLACED FWD FLOOR PANEL 222BF IAW SRM 51-10-02-0G-0 PARA 9A AND AIPC 53-21-51-21L ITEM 135. 57066U 5/5/21SDR SWAA2021062370059Floor Panel · damagedAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS. / DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 241AAF IAW SRM 51-10-02-0G-0 PARA 9A AND AIPC 53-21-00-26 ITEM 150. 57066U 5/5/21SDR SWAA2021062369135Floor Panel · damagedAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS. / AREAS OF PULLED STRANDS ON UPPER SURFACE OF AFT FLOOR PANEL 242UF WAS REPAIRED IAW SRM 53-00-50-2R-1 56563R 11MAY21SDR SWAA2021062369134Floor Panel · damagedAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS. / DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 242TF IAW SRM 51-10-02-0G-0 PARA 9A AND AIPC 53-21-00-26 ITEM 96. 57066USDR SWAA2021062369133Floor Panel · damagedAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. / DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 2412F IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 76 57066U 5/5/21SDR SWAA2021062369132Floor Panel · damagedAFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS. / DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 241YF IAW SRM 51-10-02-0G-0 PARA 9A AND AIPC 53-21-00-26 ITEM 66. 57066U 5/5/21SDR SWAA2021062369131Floor Panel · damagedAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. / AREAS OF PULLED STRANDS ON UPPER SURFACE OF AFT FLOOR PANEL 241XF WAS REPAIRED IAW SRM 53-00-50-2R-1. 56563R 12MAY21SDR SWAA2021062369130Floor Panel · damagedAFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS. / AFT FLOOR PANEL 241 AEF WITH PULLED STRANDS ON UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG. # 147A5810 SHEET # 351. 59702U 05/08/21SDR SWAA2021062369129Floor Panel · damagedAFT FLOOR PANEL 241ADF UPPER O/B EDGE IS DAMAGED. / DUE TO THE EXTENT OF DAMAGE REPLACED AFT FLOOR PANEL 241ADF IAW SRM 51-10-02-0G-0 PARA 9A AND AIPC 53-21-00-26 ITEM 250. 57066U 5/5/21SDR SWAA2021062368917Bulkhead · crackedREPAIR CRACK ON B.S. 663 LOWER COMPOSITE BULKHEAD AT R.B.L. 50; W.L. 158. / REPAIRED CRACK ON B.S. 663 LOWER COMPOSITE BULKHEAD AT R.B.L. 50; W.L. 158 PER SRM 51-70-04-2R-10.SDR SWAA2021062368916Skin · delaminatedFLAP TRACK FAIRING 543AB HAS A DELAMINATION ON THE OUTER SKIN JUST AFT OF THE LEADING EDGE / REPAIRED DELAMINATION ON THE OUTER SKIN JUST AFT OF THE LEADING EDGE ON FLAP TRACK FAIRING 543AB IAW SWA EA 21-157-01309 REV: IR AND ATS ER 21-01852 REV: IR.SDR SWAA2022030179129Web · corroded***CORROSION*** AFT CARGO DOOR SURROUND STRUCTURE BS 787+5-847 RBL 24.5 WL157 SUBWEB THRESHOLD; SEVERAL AREAS HAS CORROSION. / REJECTED REJECTION INSP 52 27MAY21 REPLACED 2 EA FASTENERS IAW SRM 51-40-02; DWG 146A8340 92964U 05/28/21SDR SWAA2021062368915Support · corroded***CORROSION*** BS 947 WL157 RBL24-LBL9 AFT BULKHEAD PANEL SUPPORT HAS CORROSION. / REMOVED AND REPLACED ACB AFT BULKHEAD SUPPORT B/S 947 RBL 24 - LBL 9 PER SRM 51-40-02-0G-0; DWG # 149A8110; DWG # 149A8117.SDR SWAA2021062368913Support · corroded***CORROSION*** BS 847-867 RBL24.5 WL157; SIDEWALL PANEL SUPPORT SHIELD HAS CORROSION. / NO ALLOWABLE DAMAGE FOUND IN B737-700 SRM FOR SUPPORT SHIELD. REPAIR BY REPLACEMENT IAW SRM 51-10-02; PARA 9C. REMOVED DAMAGED SHIELD IAW SRM 51-40-02. LOCATED; DRILLED ANSDR SWAA2021062368911Shield · corroded***CORROSION*** BS 767-787 RBL24.5 WL157 SIDEWALL PANEL SUPPORT SHIELD HAS CORROSION. / NO ALLOWABLE DAMAGE FOUND IN B 737-700 SRM FOR SUPPORT SHIELD. REPAIR BY REPLACEMENT IAW SRM 51-10-02; PAR 9C. REMOVED DAMAGED SHIELD IAW SRM 51-40-02. LOCATED; DRILLED ANDSDR SWAA2021062368909Support · corroded***CORROSION*** ACB BS 747-767 RBL24 WL157; UNDERNEATH SIDEWALL PANEL SUPPORT BAFFEL HAS CORROSION. / NO ALLOWABLE DAMAGE FOUND FOR THIS PART IN B737-700 SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02; PARA 9C. REMOVED DAMAGED PART IAW SRM 51-40-02. LOCATED; DRILSDR SWAA2021062368908Support · corroded***CORROSION*** ACB BS 727B-767 RBL21 WL157; SIDEWALL PANEL SUPPORT SEVERAL AREAS HAS CORROSION. / REMOVED SEVERAL AREAS OF CORROSION IAW SRM 51-10-02. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. RECEIVED NEW PART FROM 5 STORES. REF: PO 818957. LOCATED;SDR SWAA2021062368905Skin · crackedUPON COMPLETION OF CCN; 15029 #2; FOUND 1 INCH CRACK AT R/H HORIZONTAL STAB. LWR SKIN COMMON TO THE 193.90 RIB; 18 INCHES FROM THE FRONT SPAR. AREA MARKED / REPAIRED 1 INCH CRACK AT R/H HORIZONTAL STAB LWR SKIN COMMON TO THE 193.90 RIB; 18 INCHES FROM THE FRONSDR SWAA2021062368904Scuff Plate · crackedFWD CARGO DOOR WAY AFT CORNER SCUFF PLATE CRACKED / REPAIRED FWD CARGO DOOR AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1SDR SWAA2021062368900Stiffener · crackedLEFT HAND STABILIZER INSPAR RIB AT STAB STA. 129.50 3RD STIFFENER IS CRACKED / REMOVED CRACK DAMAGE AT LEFT HAND STABILIZER INSPAR RIB AT STAB STA. 129.50 3RD STIFFENER FROM FRONT SPAR AND INSTALLED REPAIR IAW SRM 55-10-09-2R-4 REPAIR 4 FIG 202 DETAIL A.SDR SWAA2021062368897Stiffener · crackedRIGHT HAND HORIZONTAL STAB INSPAR RIB AT STAB STA. 120.30 FOURTH STIFFENER IS CRACKED / REPAIRED RIGHT HAND HORIZONTAL STAB INSPAR RIB AT STAB STA. 120.30 FORTH STIFFNER PER SRM 55-10-09-2R-4SDR SWAA2021062368896Stiffener · crackedRIGHT HAND HORIZONTAL STAB INSPAR RIB AT STAB STA. 120.30 THIRD STIFFENER IS CRACKED / REPAIRED RIGHT HAND HORIZONTAL STAB INSPAR RIB AT STAB STA 120.30 THIRD STIFFNER PER SRM 55-10-09-2R-4SDR SWAA2021062368895Stiffener · crackedRIGHT HAND HORIZONTAL STAB INSPAR RIB AT STAB STA. 120.30 SECOND STIFFENER IS CRACKED / REPAIRED RIGHT HAND HORIZONTAL STAB INSPAR RIB AT STAB STA 120.30 SECOND STIFFNER PER SRM 55-10-09-2R-5SDR SWAA2021062368894Fairing · crackedRIGHT HORIZONTAL STAB T/E PANEL 343DB AFT FAIRING STRIP IS CRACKED / REMOVED AND REPLACED OPT FAIRING STRIP OF RIGHT HORIZONTAL STAB T/E PANEL #343DB IAW DWG 185A1702 AND SRM 51-40-02-0G-0 60215U 04JUN21SDR SWAA2021062368893Skin · debondedL/H O/B AFT FLAP I/B END LOWER SURFACE HAS A DISBOND / REMOVED AND REINSTALLED L/H O/B AFT FLAP IAW AMM 27-51-22-000-801 AND AMM 27-51-22-400-801 AND PERFORMED FUNCTIONAL TEST ALL TESTS GOOD (POS:L/H O/B; TAG NO:793983; P/N OFF/ON:113A3700-21; S/N OFF/ON:00159SDR SWAA2021062368400Bulkhead · crackedB.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT R.B.L. 50; W.L. 158. / REMOVED R/H VAPOR BARRIER BS 663 IAW SRM 51-40-02; REPAIRED R/H VAPOR BARRIER ON W/C U 314243; RE-INSTALLED R/H VAPOR BARRIER IAW SRM 51-40-02; DWG 111A1000 REV.A; DWG 111A1001 REV. A. APPLSDR SWAA2021062368388Stiffener · crackedB.S. 663 LOWER COMPOSITE BULKHEAD VERTICAL 'L' ANGLE STIFFENER IS CRACKED AT L.B.L. 26; W.L. 150; ON AFT SIDE OF B.S. 663 BULKHEAD. / REMOVED AND REPLACED B.S. 663 LOWER COMPOSITE BULKHEAD VERTICAL 'L' ANGLE STIFFINER AT L.B.L 26; W.L. 150; ON AFT SIDE OF B.S.SDR SWAA2021062367182Skin · crackedPOSSIBLE CRACK AT FASTENER AT #7 SLAT LOWER SURFACE OF THE LEADING EDGE SLAT SKIN AT ACTUATOR RIB. / REPAIRED CRACK AT FASTENER AT #7 SLAT LOWER SURFACE OF THE LEADING EDGE STAT SKIN AT ACTUATOR RIB PER SRM 57-42-01-2R-8SDR SWAA2021040761520Lamp · inoperativeL/H FWD EMERGENCY LIGHT INOP... / RE-LAMPED L/H FWD EMERGENCY LIGHT REF AMM: 33-51-04; NO DEFECTS NOTED.SDR SWAA2021022551084Sensor · faultyFLAPS DID NOT RAISE FROM FLAP #1 AFTER TAKEOFF. COMPLIED WITH QRH FOR FLAPS DISAGREE. PERFORMED ALTERNATE FLAP LADNING. NO LIMITS EXCEEDED / FOUND FSEU FAULT CODE 27-52260 (TE FLAP SENSOR RIGHT). R/R FLAP SKEW DETECTION SENSOR PER MM 27-59-01 REF LG PG 1354453SDR SWAA2021022450996Transmitter · faulty"TAKEOFF CONFIG" LIGHT ILLUMINATED AND TO HORN SOUNDED AFTER V1 AT 130 KTS. STAYED ILLUMINATED AND SOUNDING UNTIL THE LANDING GEAR CLEARED THE GROUND. / FOUND FSEU FAULT CODE 27-52261. R/R RIGHT FLAP POSITION TRANSMITTER PER MM 27-58-01. RAR # 89058 ASSISTED BSDR SWAA2021021548402Pin · dirtyFO SEAT WILL NOT LOCK IN IN HORIZONTAL TRACK / REMOVED DEBRIS FROM SEAT LOCK PINS; OPS CK GOOD REF M/M 25-11-01SDR SWAA2021021548176Cover · looseEXIT SIGN COVER NEEDS TO BE RE-ATTACHED NEAR EMERGENCY EXIT ROW / RE-INSTALLED EXIT SIGN LENS COVER PER AMM 33-51-01. LOCATED IN CTR AISLE NEAR ROW 10.SDR SWAA2020050446249Seat Track · defectiveMECHANIC REPORTS F/O'S I/B AFT SEAT TRACK HOLES FAILED CHECK. / R&R F/O'S I/B AFT SEAT TRACK PER M/M 25-11-11SDR SWAA2020050446248Seat Track · defectiveMECHANIC REPORTS CAPTAINS I/B AFT SEAT TRACK HOLES FAILED CHECK. / R&R CAPTAINS I/B AFT SEAT TRACK PER M/M 25-11-11SDR SWAA2021081846234Seal · crackedLEFT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / REMOVED AND REPLACED LEFT HORZ STAB UPPER FWD SLIDING SEAL PER AMM 53-31-31SDR SWAA2021050646235Seal · crackedRIGHT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / REMOVED AND REPLACED RIGHT HORIZ STAB UPPER FWD SLIDING SEAL PER AMM 53-31-31.SDR SWAA2020012940856Sign · damagedFORWARD SERVICE DOOR EXIT SIGN ON GALLEY DAMAGED / R&R LIGHT ASSEMBLY IAW AMM.SDR SWAA2019110638647Cover · brokenSUPPLEMENTAL INFORMATION-----------------------------------------------AFT GALLEY EMERGENCY EXIT LIGHT SWITCH COVER BROKEN. SWITCH OPERATES NORMALLY. / INSTALLED AFT GALLEY EMERGENCY LIGHT SWITCH COVER PER SIP.SDR SWAA2019091036745Light · inoperativeRT OVERWING EMERGENCY SIDEWALL LIGHT INOP. RELAMPED LIGHT IAW PER MM.SDR SWAA2019052232907Connector · disconnectedRT OVERWING EMERGENCY EXIT FLOOR PROXIMITY LIGHT INOP. RECONNECTED CONNECTOR IAW WDM.SDR SWAA2022030966168Support Bracket · crackedAFT SERVICE DOOR; LWR GATE INNER COVER AFT SUPT BRKT CRACKED. / REPLACED AFT SERVICE DOOR PAN ASSY WHICH INCLUDE THE CRACKED BRACKET IAW B737 SRM 51-40-02. A TAG:WN877.SDR SWAA2022030966160Angle · crackedSWA WORK CARD #14020-57; STEP 2.D.: .300' CRACK IN BS 663 MLG PRESS. BULKHEAD ATTACH ANGLE FROM DRAIN HOLE TO I/B DOME NUT ATTACH FASTENER HOLE; BS 663; LBL 35; WL 195; AREA MARKED IN BLACK; CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS / REPAIRED STA 663 LOWER SDR SWAA2022022466104Flap · delaminatedLH WING O/B AFT FLAP HAS DELAM AT INBOARD END NEXT TO PREVIOUS REPAIR / REPAIRED L/H WING O/B AFT FLAP ON UPPER SURFACE I/B CORNER IAW SRM 51-70-10-2R-4 AND SRM 51-70-10-2R-0SDR SWAA2019051732789Pressure Panel · crackedVERTICAL PRESSURE WEB INTERNAL CRACKED AT BS. 663, RBL 42. REPAIRED WEB IAW SRM.SDR SWAA2019051532713Beam · crackedR1 DOOR NR 4 BEAM CRACKED IN RADIUS. R&R NR 4 BEAM IAW EO # 52-41-14093.SDR SWAA2022030165874Bracket · crackedRIGHT WING UPPER SURFACE ACOSS PANEL 651AT. I/B STABILIZER LINK ASSY FWD ATTACHMENT BRACKET IS CRACK / REMOVED AND REPLACED BRACKET AT RH WING UPPER SURFACE ACCESS PNL 651AT IB STABILIZER LINK ASSY FWD ATTACHMENT REF SRM 51-40-02SDR SWAA2019012128634Support Fitting · corrodedRT MAIN LANDING GEAR TRUNNION SUPPORT FITTING LOWER INBOARD LUG BORE OUTER SURFACE OF THE FITTING CORRODED. REPAIRED FITTING PER EA.SDR SWAA2019012128633Support Fitting · corrodedRT MAIN LANDING GEAR TRUNNION SUPPORT FITTING UPPER INBOARD LUG BORE OUTER SURFACE OF THE FITTING CORRODED. REPAIRED FITTING PER EA.
Back to N938WN