Boeing 767-3S2F
Service difficulty reports · 2,378
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 = '7673S2F' 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 = '7673S2F' 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 FDEA202101170143Attach Angle · crackedNR 2 PYLON AFT BULKHEAD TO AFT FAIRING INBOARD ATTACH CLIP IS CRACKED AT APPROXIMATELY NAC STA LT. REMOVED OLD CLIP AND INSTALLED NEW CLIP, IAW BAC DWG 313T2310 REV.SDR FDEA202101170141Former · crackedRT WING LEADING EDGE NOSE FORMER CRACKED AT APPROXIMATELY OSS490. REMOVED OLD AND INSTALLED NEW NOSE FORMER, IAW BAC DWG 114T2511 REV D AND FED EX EA H-5720-TO359038 P1.SDR FDEA202101170140Former · crackedLT WING LEADING EDGE FORMER CRACKED APPROXIMATELY OSS490. REMOVED OLD AND INSTALLED NEW NOSE FORMER, IAW BAC DWG 114T2511 REV D AND FED EX EA H-5720-TO 359039.SDR FDEA202101170138Former · crackedLT WING LEADING EDGE NOSE FORMER CRACKED APPROXIMATELY OSS435. FABRICATED NEW NOSE FORMER AND INSTALLED, IAW BAC DWG 114T2171, REV- & EA H-5720- TO 359037.SDR FDEA202101160130Former · crackedRT WING FIXED LEADING EDGE FORMER IS CRACKED AT OFSS 436. REMOVED AND REPLACED P/N 114T2170-6 AND 114T2171-3, IAW B767 SRM 51-40-02 AND FEDEX EA H-5720-T039040 P1.SDR FDEA202101150129Former · crackedRT WING FIXED LEADING EDGE FORMER CRACKED AT APPROXIMATELY OSS663. REMOVED OLD AND INSTALLED NEW NOSE FORMER, IAW BAC DWG 114T2512 AND FED EX EA H- 5720-T0359036.SDR FDEA202101150126Skin · damagedNR 5 SLAT TRAILING EDGE LOWER SURFACE HAS GOUGE OUTBOARD OF OUTBOARD MAIN TRACK. REPAIRED NR 5 SLAT TRAILING EDGE LOWER SURFACE OUTBOARD MAIN TRACK, IAW B767 SRM 57-43-02-2R, 51-20-10-2R AND 51-20-05-06.SDR FDEA202101150125Skin · gougedNR 5 SLAT TRAILING EDGE LOWER SURFACE HAS GOUGE OUTBOARD OF INBOARD AUX TRACK. REPAIRED IAW B767 SRM 57-43-02-2R FIG 201 AND SRM 51-70-10-2R. APPLIED FILLET SEAL, IAW SRM 51-70-10-2R PAR 22 AND SRM 51-20-05-0G.SDR FDEA202101140102Panel · wornLEFT WING INBOARD AILERON REMOVABLE LEADING EDGE PANEL HAS EXPOSED COMPOSITE. REPAIRED LEFT WING INBOARD AILERON REMOVABLE LEADING EDGE PANEL, IAW B767 SRM 57-60-01-2R AND 51- 70-17-0G PARA 4G.SDR FDEA202101130087Skin · gougedLT WING NR 4 SLAT TRAILING EDGE WEDGE LOWER SURFACE HAS GOUGE INBOARD OF INBOARD MAIN TRACK FROM FASTENER ON FIXED LEADING EDGE UPPER SURFACE. REPAIRED NR 4 SLAT TRAILING EDGE WEDGE LOWER SURFACE GOUGE WITH 250 DEGREE METAL BOND REPAIR, IAW B767 SRM 57-43-02-SDR FDEA202101130078Skin Splice · crackedRIGHT WING FIXED LEADING EDGE SKIN SPLICE STRAP IS CRACKED AT APPROXIMATELY OSS 514.167. REMOVED AND REPLACED RT WING LEADING EDGE SKIN SPLICE STRAP P/N 114T2800-165, IAW B767 SRM 51-40-02 AND BAC DWG 114T2800 REV C.SDR FDEA202012153166Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241YFA MISSING EDGE FILLER AT LBL 54. FABRICATED NEW FLOOR PANEL 241YFA, IAW FEDEX DWG SRZ-25-005 REV C.SDR FDEA202012153167Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242SFF HAS SEVERAL AREAS OF DELAMINATION AND CRUSH DAMAGE AROUND FLOOR FITTING CUTOUTS. FABRICATED NEW FLOOR PANEL 241SFF, IAW FEDEX DWG SRZ-25-005, REV R.SDR FDEA202012153165Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242TFA IS PUNCTURED TWO PLACES. FABRICATED NEW FLOOR PANEL 242TFA, IAW FEDEX DWG SRZ-25-005, REV R.SDR FDEA202012153164Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241ZFF HAS CRUSH AND DELAM DAMAGE, SEVERAL AREAS ALONG THE ENTIRE LENGTH. FABRICATED NEW FLOOR PANEL 241ZFF, IAW FEDEX DWG SRZ-25-005, REV R.SDR FDEA202012153163Floor Support · crackedRT AFT FUSELAGE, AFT CARGO BS 1576 RBL 78, MAIN CARGO DECK FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE RIGHT AFT FUSELAGE MAIN CARGO DECK FLOOR SUPPORT SPLICE ANGLE AT STA 1576 AND RBL 78, IAW BAC DWG 146T5650, REV C AND B767 SRM 51-40-02-0G.SDR FDEA202012153162Floor Support · crackedLT AFT FUSELAGE, AFT CARGO BS 1576 LBL 78, MAIN CARGO DECK FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE LEFT AFT FUSELAGE MAIN CARGO DECK FLOOR SUPPORT SPLICE ANGLE AT STA 1576 AND LBL 78, IAW BAC DWG 146T5650, REV C AND B767 SRM 51-40-02-0G.SDR FDEA202012143155Switch · out of toleranceAT FL380 EICAS MAIN CARGO DOOR ILLUMINATED FOLLOWED QRH PROCEDURES & LANDED. LIGHT EXTINGUISHED PASSING 16,000 IN DECENT. NO CABIN DEPRESSURIZATION OR NOISE FROM CARGO DOOR. ON BOARDING ACFT FOUND BOTH DOOR LATCHED AND DOOR LOCKED INDICATIONS SHOWING GRSDR FDEA202012093082Skin · chafedRIGHT WING NR 9 SLAT LOWER TRAILING EDGE WEDGE SKIN CHAFED. REPAIRED NR 9 SLAT RIGHT WING LOWER TRAILING EDGE WEDGE 33.75" FROM INBOARD END BY BONDING FILLER SKIN, INTERNAL DOUBLER, CORE, FIBERGLASS WEDGE AND EXTERNAL DOUBLER, IAW B767 SRM: 57-43-02-2R REPAISDR FDEA202012093079Former · crackedLT WING LEADING EDGE, FORM P/N 114T2170-5 CRACKED AT OUTBOARD SIDE OF THE INBOARD AUX TRACK OF THE NR 5 SLAT BETWEEN WS 433 AND 460, STREAMER ATTACHED. REMOVED AND REPLACED NOSE FORMER PN 114T2127-4 ON LT WING STA OSS441, PER FEDEX EA: H-5720-T0358462-P1. TISDR FDEA202012093078Slat System · malfunctionedPDIS 109 27-80 5999 09DEC20 DUB OPEN U LOGPAGES:371455. LEADING EDGE SLAT ASYM EICAS MESSAGE LIGHT WITH LEADING EDGE LIGHT FLAP GAUGE INDICATIONG BETWEEN 1 AND UP. NO CONTROL ISSUES NOTED INDICATED. POSITION PROPERLY ON EXTENSION PER QRH. SHGN 09DEC20 07:0SDR FDEA202012083074Former · crackedLT WING LEADING EDGE 1 EACH FORM CRACKED AT THE OUTBOARD SIDE OF ROTARY ACTUATOR OF THE NR 5 SLAT BETWEEN WS 486.2 AND 512.2 STREAMER ATTACHED. REMOVED AND REPLACED NOSE FORMER AT OSS 499, PER BAC DWG 114T2161 REV B FEDEX B767 SRM 51-40-02 AND FEDEX EA H-5720SDR FDEA202012083073Former · crackedLT WING LEADING EDGE FORM P/N 114T2170-3 CRACKED AT INBOARD SIDE OF INBOARD AUX TRACK OF NR 5 SLAT BETWEEN WS 433 AND 460. STREAMER ATTACHED FABRICATED FORMER LT WING LEADING EDGE PN 114T2170-3 AT INBOARD SIDE OF INBOARD AUX TRACK, IAW BAC DWG 114T2170. INSTSDR FDEA202012083069Skin · delaminatedRIGHT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE IS DELAMINATED 2" FORWARD OF TRAILING EDGE AND 7" INBOARD OF THE OUTBOARD EDGE. REPAIRED RIGHT WING INBOARD TRAILING EDGE AFT FLAP LOWER SURFACE, IAW B767 SRM 57-53-01-2R FIGURE 201 DETAIL 3, 51-70-10-2R REPSDR FDEA202012083072Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241NFF HAS BROKEN INSERTS AND DELAMINATION DAMAGE ALONG THE FORWARD EDGE. FABRICATED NEW MAIN CABIN FLOOR PANEL 241NFF, IAW FEDEX DWG SRZ-25-005 REV R.SDR FDEA202012083071Floor Panel · damagedMAIN CABIN FLOOR PANEL 241JFF HAS CRUSH AND DELAMINATION DAMAGE ALONG THE LBL 55 SIDE, ENTIRE LENGTH. FABRICATED NEW MAIN CABIN FLOOR PANEL 241JFF, IAW FEDEX DWG SRZ-25-005, REV R.SDR FDEA202012083070Floor Panel · damagedMAIN CABIN FLOOR PANEL 241WFF HAS THREE SEPARATE AREAS OF DAMAGE. REPAIRED 3 EA DAMAGE AREAS ON FLOOR PANEL 241WFF, IAW B767 SRM 53-00-50-2R, PARA 4C.SDR FDEA202012073171Beam · damagedNR 2 PYLON INBOARD SKIRT BEAM FWD FLANGE HAS ELONGATED HOLES. REPAIRED ELONGATED HOLES ON NR 2 PYLON INBOARD SKIRT BEAM FWD FLANGE, IAW FEDEX EA H-5450-T0358609-P1.SDR FDEA202012073056Floor Panel · damagedMAIN CABIN FLOOR PANEL 241HFF HAS MISSING EDGE FILLER SEVERAL AREAS. REPAIRED EDGE FILLER ON FLOOR PANEL 241HFF, IAW B767 SRM 53-00-50-2R PARA 4G (2).SDR FDEA202012063051Angle · crackedFWD LT FRAME STA 246 LBL 50 BELOW FLOOR INTERCOSTAL ANGLE CRACKED. REMOVED AND REPLACED ANGLE P/N 141T5146-16, IAW B767 SRM 51-40-02 AND BAC DWG 141T5600 REV-.SDR FDEA202012053039Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242BFA IS PUNCTURED TWO PLACES. REPAIRED DAMAGES TO FLOOR PANEL 242BFA, IAW B767 SRM 53-00-50-2R, PARA 4C.SDR FDEA202012053038Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241LFF PUNCTURED TWO PLACES AND HAS MISSING EDGE FILLER. REPAIRED DAMAGES TO FLOOR PANEL 241LFF, IAW B767 SRM 53-00-50-2R, PARA 4C AND 4G (2).SDR FDEA202012053037Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241FFF PUNCTURED THREE PLACES. REPAIRED DAMAGES TO FLOOR PANEL 241FFF, IAW B767 SRM 53-00-50-2R, PARA 4D AND 4E.SDR FDEA202012053036Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242VFF HAS A PUNCTURE. REPAIRED FLOOR PANEL 242VFF, IAW B767 SRM 53-00-50-2R, PARA 4D.SDR FDEA202012053035Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242HFF IS PUNCTURED, MARKED. REPAIRED FLOOR PANEL 242HFF, IAW B767 SRM 53-00-50-2R, PARA 4C.SDR FDEA202012053033Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241KFF IS DAMAGED AT 3 SEPARATE AREAS, MARKED. REPAIRED 3 EA DAMAGES ON FLOOR PANEL 241KFF, IAW B767 SRM 53-00-50-2R, PARA 4C AND 4D.SDR FDEA202012053032Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241QFF HAS PUNCTURE DAMAGE, MARKED. REPAIRED FLOOR PANEL 241QFF, IAW B767 SRM 53-00-50-2R, PARA 4D.SDR FDEA202012033020Bracket · crackedLT WING INBOARD FIXED LEADING EDGE, 1 EACH TORQUE TUBE BRACKET CRACKED APPROXIMATELY LES 285. STREAMER ATTACHED, REMOVED AND REPLACED BRACKET, IAW BAC DWG 114T1240 REV E AND B767 SRM 51--40-02.SDR FDEA202012013025Attach Angle · crackedNR 1 PYLON AFT FAIRING, OUTBOARD FRAME ATTACH CLIP IS CRACKED AT NAC STA 376 LT. REMOVED AND REPLACED CLIP, IAW B767 SRM 51-40-02.SDR FDEA202011293053Frame · crackedNR 2 PYLON CENTER FITTING AT STA 329 INBOARD SIDE CRACKED. ACCOMPLISHED FRAME CRACK REPAIR AT NAC 329, IAW B767 SRM 54-52-71-2R.SDR FDEA202011242958Former · crackedLT WING NOSE FORMER AT STA OSS 441, OUTBOARD TRACK IS CRACKED. REMOVED AND REPLACE NOSE FORMER ASSEMBLY, PER B767 SRM 51-40-02 & BOEING DWG 114T2170-5 REV A & FEDEX EA NR: H-5720-T0358170A P1. TITLE: WINGS-SECONDARY WING STRCT-LT WING, LEADING EDGE, ANGLE, OSDR FDEA202011222944Former · crackedLT WING LEADING EDGE BRACKET CRACKED STA 286. REMOVED AND REPLACED NOSE FORMER AND ANGLE, PER FEDEX EA H-5720-T0358268-P1. TITLE: WINGS-SECONDARY WING STRCT-LT WING, LEADING EDGE, ANGLE, OSS 437 ALTERNATE FASTENERS, AND BAC DWG 114T2241 REV.SDR FDEA202011202933Floor Panel · damagedMAIN CABIN FLOOR PANEL 241FFF HAS TWO SMALL AREAS OF DAMAGE. REPAIRED FLOOR PANEL 241FFF, IAW B767 SRM 53-00-50-2R, PARA 4C.SDR FDEA202011202932Floor Panel · damagedMAIN CABIN FLOOR PANEL 241LFF HAS TWO SMALL AREAS OF DAMAGE. REPAIRED FLOOR PANEL 241LFF, IAW B767 SRM 53-00-50-2R, PARA 4C.SDR FDEA202011202931Floor Panel · damagedMAIN CABIN FLOOR PANEL 241ZFF HAS ONE SMALL AREA OF DAMAGE. REPAIRED FLOOR PANEL 241ZFF, IAW B767 SRM 53-00-50-2R, PARA 4C.SDR FDEA202011202930Floor Panel · damagedMAIN CABIN FLOOR PANEL 241XFF HAS A SMALL HOLE. REPAIRED FLOOR PANEL 241XFF, IAW B767 SRM 53-00-50-2R, PARA 4C.SDR FDEA202011202929Floor Panel · damagedMAIN CABIN FLOOR PANEL 241AFF HAS DAMAGE 2 PLACES. REPAIRED FLOOR PANEL 241AFF, IAW B767 SRM 53-00-50-2R, PARA 4E.SDR FDEA202011202928Floor Panel · damagedMAIN CABIN FLOOR PANEL 241DFF HAS PUNCTURE DAMAGE. REPAIRED FLOOR PANEL 241DFF, IAW B767 SRM 53-00-50-2R, PARA 4C.SDR FDEA202011202927Floor Panel · damagedMAIN CABIN FLOOR PANEL 241DFF IS DAMAGED AT STA 759 AND LBL 61.5. REPAIRED FLOOR PANEL 241DFF, IAW B767 SRM 53-00-50-2R, PARA 4E.SDR FDEA202011202926Floor Panel · damagedMAIN CABIN FLOOR PANEL 241AFF IS DAMAGED AT STA 752 AND LBL 7. REPAIRED FLOOR PANEL 241AFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
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