Boeing 737-277
Service difficulty reports · 1,584
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 = '737277' 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 = '737277' 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 AWXA200301394Skin · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK A .75 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FASTENER HOLE ON FORWARD UPPER CORNER OF R-1 DOOR, BS 292.50. MAINTENANCE PERFORMED HFEC ON CRACK AND IDENTIFIED CRACK END; STOP DRILLED CRACK IN FUSELAGE SKIN AT R-1 DOOR FSDR AWXA200301262Battery Pack · dischargedDURING INSPECTION THE L-2 & R-2 DOOR EMERGENCY EXIT EXTERIOR LIGHTS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT ESCAPE SLIDES BATTERY BACK IN THE AFT CARGO COMPARTMENT BS 920 IAW BMM 33-51-71, OPERATIONAL CHECK C/W IAW BMM 33-51-11.SDR AWXA200301208Wire · brokenDURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13 & 14 LT WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN SPLICE ON EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301207Wire · wornDURING INSPECTION THE OVER WING EMERGENCY EXIT AISLE SIGN WAS FOUND INOPERATIVE ON ONE SIDE. MAINTENANCE RE-PINNED THE BACK SHELL CONNECTOR ON OVER WING EMERGENCY EXIT AISLE SIGN, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301206Pump · inoperativeON CLIMB OUT OF PHX EN ROUTE FOR SJC LOST (A) SYS HYDS, TURNED BACK TO PHX & LANDED WITHOUT EVENT. MAINT R & R NR 2 EDP IAW T/C R5M29001. R & R (A) HYD SYS CASE DRAIN, PRESSURE, & RETURN FILTERS, FLUSHED SYSTEM IAW BMM 29-11-0, PG. 204. LEAK AND OPERATIONAL CHSDR AWXA200301473Frame · crackedLCQ - MAJOR REPAIR - DURING C-14 CHECK 2 EACH CRACKS WERE FOUND IN FASTENER HOLES ON THE RT FUSELAGE FRAME AT BS 727, BETWEEN WL 195 AND WL 202. MAINTENANCE OVERSIZED HOLES AND PERFORMED HFEC INSPECTION TO VERIFY CRACKS CONTAINED, NO CRACK INDICATIONS WERE NOSDR AWXA200301095Line · leakingDURING DECENT INTO DFW EN ROUTE FROM PHX (A) SYSTEM HYDRAULIC QUANTITY INDICATOR BEGAN SHOWING LOSS OF FLUID. FLUID LEVEL DROPPED TO APPROX .7500 OF A GAL REMAINING. EMERGENCY EQUIPMENT CALLED OUT AS A PRECAUTION. MAINTENANCE FOUND THE NOSE LANDING GEAR ACTUASDR AWXA200301086Wire · brokenDURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301077Battery · dischargedFLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT IN THE AFT GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN AFT GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301060Panel · crackedDURING C-16 CHECK .1875 INCH CRACK WAS FOUND ON CLOSE OUT PANEL BELOW NR 2 SLAT INBOARD MAIN TRACK AT WBL 355. MAINTENANCE REMOVED CRACKED NR 2 SLAT CLOSE OUT PANEL AT WBL 355; FABRICATED A NEW REPLACEMENT PANEL IAW DWG 69-53316; INSTALLED REPAIR PART IAW B737SDR AWXA200301057Garlock Seal · failedON CLIMB OUT OF PHX EN ROUTE FOR BOI THE NR 1 GENERATOR TEMPERATURE WENT INTO THE YELLOW FOLLOWED BY A GENERATOR HIGH TEMPERATURE LIGHT, ATTEMPT APU START WITH NO SUCCESS. FOLLOWED QUICK REFERENCE HANDBOOK AND DISCONNECTED THE NR 1 GENERATOR, TURNED BACK TO PHSDR AWXA200301046Clip · crackedDURING C-16 CHECK A .1250 CRACK WAS FOUND IN RADIUS OF NR 1 ENGINE LT FIXED FAIRING CLIP AT AFT END, 1ST RIB. MAINTENANCE REMOVED CRACKED CLIP ON NR 1 ENGINE LT FIXED FAIRING AFT END, 1ST RIB; FABRICATED A NEW REPLACEMENT CLIP IAW DWG 65-52263; INSTALLED REPAISDR AWXA200301045Gusset · crackedDURING C-16 CHECK A .1250 INCH CRACK WAS FOUND AT FASTENER HOLE ON NR 1 ENGINE FIXED FAIRING COVER PLATE (GUSSET) AT AFT END, 1ST RIB. MAINTENANCE REMOVED CRACKED GUSSET ON NR 1 ENGINE FIXED FAIRING AFT END, 1ST RIB; FABRICATED A NEW REPLACEMENT GUSSET IAW DWSDR AWXA200301062Battery Pack · dischargedDURING C-16 CHECK, FUNCTIONAL CHECK OF EMERGENCY EVACUATION LIGHT SYSTEM FOUND THE RT OVER WING, RT AND LT EMERGENCY ESCAPE SLIDE, AND RT AFT WING (EXTERNAL) LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT OVER WING, AND RT AFT CARGO COMPARTMENT EMSDR AWXA200301030Circuit Breaker · inoperativeON APPROACH INTO PHX EN ROUTE FROM BUR AFTER LANDING GEAR EXTENSION THERE WAS NO LANDING GEAR DOWN AND LOCKED OR UNSAFE GEAR INDICATIONS, ABORTED APPROACH. FOUND CIRCUIT BREAKER (SECT5) EXTENDED, AFTER DISCUSSION WITH MAINTENANCE CONTROL, CIRCUIT BREAKER WAS RSDR AWXA200301047Angle · crackedDURING C-16 CHECK A .3125 INCH CRACK WAS FOUND AT FASTENER HOLE ON L ANGLE AT BS 663 IN LT AFT AIR CONDITIONING BAY ABOVE TURBO FAN. MAINTENANCE REMOVED CRACKED HORIZONTAL (L) ANGLE AT BS 663; FABRICATED A NEW REPLACEMENT (L) ANGLE IAW DWG 65-45402; INSTALLED SDR AWXA200301006Valve · bindingEN ROUTE FROM ONT TO PHX AT CRUISE RECEIVED HIGH OIL TEMPERATURE LIGHT, FOLLOWED QUICK REFERENCE HANDBOOK AND SHUTDOWN THE NO. 1 ENGINE, LANDED AT PHX WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE FUEL HEAT VALVE STUCK IN THE OPEN POSITSDR AWXA200301004Wire · brokenDURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301040Angle · crackedDURING C-16 CHECK A .1875 INCH CRACK WAS FOUND ON ATTACH ANGLE AFT OF L-1 DOOR CUTOUT BS 348.20, WL 222. MAINTENANCE REMOVED CRACKED ATTACH ANGLE BS 348.20, WL 222; FABRICATED A NEW REPLACEMENT ATTACH ANGLE IAW DWG 69-26555; INSTALLED REPAIR PART IAW B737-20SDR AWXA200301053Fitting · corrodedDURING C-16 CHECK CORROSION WAS FOUND ON RT MAIN LANDING GEAR BEAM INBOARD STABILIZER FITTING AT TRAILING EDGE OF WING. MAINTENANCE REMOVED AND REPLACED CORRODED STABILIZER FITTING IAW AMM 57-01-000-4, PG. 1-2.SDR AWXA200301044Attach Angle · crackedDURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON ATTACH ANGLES AFT OF BS 348.20, LT SIDE OF FUSELAGE, WL 222. MAINTENANCE REMOVED CRACKED ATTACH ANGLE BS 348.20, WL 222; FABRICATED 2 EACH NEW REPLACEMENT ATTACH ANGLES IAW DWG'S 69-16970-501 AND 69-76555-3; INSTALSDR AWXA200301039Angle · crackedDURING C-16 CHECK A .5 INCH CRACK WAS FOUND ON WEB ANGLE JUST AFT OF BS 348.20, LT SIDE OF FUSELAGE, WL 216. MAINTENANCE REMOVED CRACKED WEB ANGLE BS 348.20; FABRICATED A NEW REPLACEMENT WEB ANGLE IAW DWG 69-16509; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-SDR AWXA200300995Light · brokenFLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300991Intercostal · crackedDURING C-16 CHECK A 3 INCH CRACK WAS FOUND ON UPPER FLANGE OF INTERCOSTAL (BAFFLE) AT BS 440-460, OUTBOARD OF STR 26 LT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL FROM BS 440 TO BS 460; FABRICATED A NEW REPLACEMENT INTERCOASTAL PER DWG 65-41473; INSTALLED REPAIRSDR AWXA200301050Connector · damagedDURING C-16 CHECK NUMEROUS CONNECTORS AND SPLICES WERE FOUND DAMAGED ON SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT HARNESS LT SIDE OF AIRCRAFT. MAINTENANCE REMOVED AND REPLACED DAMAGED CONNECTORS AND SPLICES ON SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT HARNESS LTSDR AWXA200300944Light · brokenDURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300941Controller · malfunctionedON INITIAL TAKEOFF ROLL EN ROUTE, THE CABIN CLIMB INDICATOR NEEDLE WENT TO RAPID RATE OF DESCENT OF ABOUT 4000 FPM, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER IAW BMM 21-31-21, PERFORMED OPERATIONAL CSDR AWXA200300997Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD WEB AT RBL 17.1, WL 230. PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED SDR AWXA200300996Bulkhead · crackedDURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD WEB AT LBL 17.1, WL 230. PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW SECTION OF WEB ANDSDR AWXA200301028Fairing · crackedDURING C-16 CHECK A .7500 INCH CRACK WAS FOUND ON LT WING NR 1 FLAP TRACK MOVEABLE FAIRING AT UPPER LT AFT CORNER. MAINTENANCE PERFORMED A BOND REPAIR ON LT WING NR 1 FLAP TRACK MOVEABLE FAIRING AT UPPER LT AFT CORNER IAW B737-200 SRM 51-40-09, PG. 3, 8-9.SDR AWXA200300984Stringer Clip · crackedDURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON TOP LEG OF STRINGER CLIP 22 RT, FORWARD SIDE OF BS 787. MAINTENANCE REMOVED CRACKED STRINGER CLIP 22 RT, BS 787; FABRICATED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, STEP 4SDR AWXA200300983Stringer Clip · crackedDURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON TOP LEG OF STRINGER CLIP 21 RT, FORWARD SIDE OF BS 787. MAINTENANCE REMOVED CRACKED STRINGER CLIP 21 RT, BS 787; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, STEP 4B-4E,SDR AWXA200301058Angle · corrodedDURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND AROUND NUT PLATE HOLES ON FORWARD CARGO COMPARTMENT LT TRANSITION ANGLE BETWEEN BS 380 AND BS 480. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED ANGLE BETWEEN BS 38SDR AWXA200301048Door · crackedDURING C-16 CHECK A .3125 INCH CRACK WAS FOUND ON NR 5 SLAT ACTUATOR CLOSE OUT DOOR. MAINTENANCE REMOVED CLOSE OUT DOOR ON NR 5 SLAT AT WBL 435; FABRICATED A NEW REPLACEMENT CLOSE OUT DOOR PER DWG 65C26191; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PG. SDR AWXA200301041Skin · crackedDURING C-16 CHECK A .1250 INCH CRACK WAS FOUND ON NR 3 SLAT INBOARD MAIN TRACK CLOSE OUT DOOR AT WBL 230 LT. MAINTENANCE REMOVED AND REPLACED NR 3 SLAT INBOARD MAIN TRACK CLOSE OUT DOOR ASSEMBLY AT WBL 230 LT IAW B737-200 SRM 51-30-02, PARA B & E.SDR AWXA200301023Skin · delaminatedDURING C-16 CHECK THE LT OUTBOARD HINGED FLAP TRAILING EDGE SKIN WAS FOUND DELAMINATED. MAINTENANCE PERFORMED HONEYCOMB REPAIR ON TRAILING EDGE SKIN OF LT OUTBOARD HINGED FLAP IAW B737-200 SRM 51-40-20, FIG. 10, PG. 40-41.SDR AWXA200301024Skin · delaminatedMCN - MAJOR REPAIR - DURING C-16 CHECK THE RT OUTBOARD HINGED FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED ALONG EDGE. MAINTENANCE PERFORMED HONEYCOMB REPAIR ON TRAILING EDGE WEDGE OF RT OUTBOARD HINGED FLAP IAW B737-200 SRM 51-40-20 FIG 10 PG 40-41.SDR AWXA200301019Frame · crackedDURING C-16 CHECK A 1.75 INCH CRACK WAS FOUND ON LT WING LEADING EDGE FORMER AT WS 222.7, JUST INBOARD OF NR 1 PYLON. MAINTENANCE CUT OUT DAMAGE ON LT WING LEADING EDGE FORMER AT WS 222.7 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED ASDR AWXA200301011Skin · cracked- DURING C-16 CHECK A 0.080 INCH CRACK WAS FOUND ON EDGE OF RT INBOARD HINGED FLAP UPPER SKIN AT WBL 180.75. MAINTENANCE TRIMMED OUT CRACK ON RT INBOARD HINGED FLAP UPPER SKIN AT WBL 180.75 IAW B737-200 SRM 57-50-01 PG 1 FIG 3, SHEETS 2-4.SDR AWXA200300998Frame · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A .625 INCH CRACK WAS FOUND IN RADIUS OF BS 727B FRAME AT STR 25 LT. MAINTENANCE CUTOUT DAMAGE ON BS 727B FRAME AT STR 25 LT; FABRICATED A RADIUS FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-200 SRM 5SDR AWXA200300987Beam · crackedDURING C-16 CHECK A 1/8 INCH CRACK WAS FOUND ON BEAM WEB AT INSULATION MOUNT HOLE BS 184, RBL 17.1, WL 178. MAINTENANCE CUTOUT DAMAGED AREA OF VERTICAL BEAM WEB AT BS 184, RBL 17.1, WL 178, AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACK EXISTS; FSDR AWXA200300985Attach Angle · crackedDURING C-16 CHECK A 5/8 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT SILL WEB TO FRAME ATTACH ANGLE UPPER LEG AT BS 807, RBL 19.5. MAINTENANCE REMOVED CRACKED FRAME ATTACH ANGLE AT BS 807, RBL 19.5; FABRICATED A NEW REPLACEMENT FRAME ATTACH ANGLE; INSTALLED RSDR AWXA200301059Door · crackedDURING C-16 CHECK .1250 INCH CRACK WAS FOUND ON NR 4 SLAT ACTUATOR CLOSE OUT DOOR, WBL 279.25. MAINTENANCE REMOVED CRACKED NR 4 SLAT ACTUATOR CLOSE OUT DOOR; FABRICATED A NEW REPLACEMENT DOOR; INSTALLED REPAIR PART IAW BMM 20--050-011-2, FIG. 203.SDR AWXA200301049Skin · crackedDURING C-16 CHECK A 1.250 CRACK WAS FOUND ON FUSELAGE EXTERNAL SKIN FROM FASTENER HOLE AT AFT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. MAINTENANCE CUTOUT DAMAGED SKIN AT BS 450, BL 0 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A RSDR AWXA200301052Skin · crackedDURING C-16 CHECK A .5625 INCHES CRACK WAS FOUND ON EXTERNAL FUSELAGE SKIN OF L-1 DOOR CUTOUT AT FASTENER HOLE LOWER AFT CORNER. MAINTENANCE CUTOUT CRACK ON SKIN OF L-1 DOOR CUTOUT LOWER AFT CORNER AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST;SDR AWXA200301038Skin · crackedDURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON EXTERNAL FUSELAGE SKIN AT FASTENER HOLE OF R-2 DOOR CUTOUT AT FORWARD LOWER CORNER. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED AN INNER PLATE, OUTERSDR AWXA200301022Floorbeam · crackedDURING C-16 CHECK A .5 INCH CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM AT BS 520, LBL 24. MAINTENANCE STOP DRILLED CRACK ON FLOORBEAM AT BS 520, LBL 24 AND PERFORMED HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED RESDR AWXA200301016Skin · crackedDURING C-16 CHECK A .75 INCH CRACK WAS FOUND ON LOWER LEADING EDGE OF NR 1 KRUEGER FLAP AT L/E STA 205. MAINTENANCE BLENDED OUT CRACK ON LOWER LEADING EDGE OF NR 1 KRUEGER FLAP AT L/E STA 205 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATSDR AWXA200301012Skin · crackedDURING C-16 CHECK A 0.090 INCH CRACK WAS FOUND ON R-2 DOOR EXTERNAL SKIN AT CORNER OF UPPER HINGE CUTOUT. MAINTENANCE TRIMMED OUT CRACK ON R-2 DOOR EXTERNAL SKIN AT CORNER OF UPPER HINGE CUTOUT IAW B737-200 SRM 52-00-2 PG 3, FIG 1 & 6, SHEETS 3 & 6.SDR AWXA200301010Strap · crackedDURING C-16 CHECK A .5 INCH CRACK WAS FOUND ON FLOOR STRUCTURE TIE STRAP AT BS 342, LBL 1. MAINTENANCE REMOVED CRACKED TIE STRAP AT BS 342, LBL 1; FABRICATED A NEW REPLACEMENT TIE STRAP AND A REPAIR PLATE; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-09 PG 1
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