# Service difficulty reports: N657UA

A list on [N657UA](https://openairdocs.org/aircraft/N657UA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 7 · 337 reports

- [SDR CALA2026090719285](https://openairdocs.org/sdr/CALA2026090719285.md): Wire Splice · disconnected · Sep 6, 2026 · N657UA · Boeing 767322 · Light System Wiring
  > 21AB EMERGENCY CEILING LIGHT FOUND NOT ILLUMINATING. LIGHT FOUND SPLICES SNAPPED. SPLICES REPLACED AND TEST CARRIED OUT NORMAL IAW AMM 33-51-04, AND SWPM 20-30-12.
- [SDR CALA2026042815774](https://openairdocs.org/sdr/CALA2026042815774.md): Brake · failed · Apr 25, 2026 · N657UA · Boeing 767322 · Landing Gear Brake System
  > NUMBER 5 BRAKE UNIT, CARBON PACK DAMAGED & BROKEN. EVIDENCE OF OVERHEAT DUE TO SMOKE & VISUAL HEAT DAMAGE. AMM 32-41-08/201 SERVICE TIP FOR GRABBING BRAKES. NR 5 BRAKE TEMPERATURE AT 2, NR 6 AT 1, NR 7 AT 2, NR 8 AT 2. NO ISSUES REPORTED FROM PILOTS EITHER. B
- [SDR CALA2026033014902](https://openairdocs.org/sdr/CALA2026033014902.md): Pump · faulted · Mar 27, 2026 · N657UA · Boeing 767322 · Hydraulic Pump (Electric/Engine), Main
  > R HYD QTY EICAS FOLLOW- ED BY R HYD SYS PRESS R HYD QTY READS 0FOUND HYD CASE DRAIN HOSE BLOWN. R & R HYD CASE DRAIN HOSE PER AMM SUB TASK 71-00-02-420-057-C7 WHILE LEAK CHECKING HYD CASE DRAIN HOSE DURING ENG RUN THE EDP NEVER CAME ON. R & R RT SYS RETURN F
- [SDR CALA2026021813870](https://openairdocs.org/sdr/CALA2026021813870.md): Idg · faulted · Feb 15, 2026 · N657UA · Boeing 767322 · AC Generator-Alternator
  > RIGHT GENERATOR DRIVE DISC CAUTION LIGHT. PERFORMED QRH, CREW ASSISTED TO PERFORM IDLE ENGINE RUN TO CONFIRM RT IDG DISCONNECTED. APPROVED MEL, RT ENG GEN DISCONNECTED AND SWITCHED OFF, DEFERRED IAW MEL 2400F. THERE IS HISTORH REF LP-7704551. R & R GCU AN
- [SDR CALA2025122112274](https://openairdocs.org/sdr/CALA2025122112274.md): Adc · faulted · Dec 18, 2025 · N657UA · Boeing 767322 · Air Data Computer
  > IAS DISAGREE EICAS MSG. CAPT SIDE SHOWING.785 FO SIDE SHOWING. 815 AT 340 CREW VERBAL. STAND BY IND MATCHED F/O SIDE, CAPT ADC SWITCHED TO ALT AND SYS MATCHED. PERFORMED BITE TEST ON BOTH LEFT AND RIGHT ADC COMP. WITH NO FAULTS. REQ FURTHER T/S. REF FIM 34-1
- [SDR CALA2025101309933](https://openairdocs.org/sdr/CALA2025101309933.md): Light · no test · Oct 11, 2025 · N657UA · Boeing 767322 · Emergency Lighting
  > OPERATIONAL TEST - EMERGENCY ESCAPE PATH LIGHTING (EEL) SYSTEM PERFORM OPERATIONAL CHECK - 45D AISLE EMERGENCY LIGHT IS DAMAGED. 45D AISLE EMERGENCY LIGHT REPLACED IAW AMM 33-51-10-962-104.
- [SDR CALA2025100909858](https://openairdocs.org/sdr/CALA2025100909858.md): Lens · detached · Oct 8, 2025 · N657UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY EXIT SIGN LENS DETACHED, ABOVE AISLE, NEXT TO OVERWING EMERGENCY EXIT DOOR, RT SIDE OF AIRCRAFT, AFT FACING LENS COVER. LENS AND MOUNT WERE NOT BROKEN, JUST UNCLIPPED FROM LIGHT ASSEMBLY, ASSEMBLED BACK TOGETHER IAW AMM 33-51-01-962-028. LIGHT TEST P
- [SDR CALA2025090308432](https://openairdocs.org/sdr/CALA2025090308432.md): Filter · odor · Sep 1, 2025 · N657UA · Boeing 767322 · Air Distribution System
  > MID TO AFT CABIN HAS MILD TO STRONG FOUL SMELL. REPLACE RECIRC AIR FILTERS REF IPC EQUIPMENT INSTL-CAB. AIR RECIRCULATION REFERENCE: 21-25-01-02. REMOVED AND REPLACED BOTH RECIRC AIR FILTERS PER AMM 21-25-02. PERFORMED OPS CHECK, REF AMM 21-25-02. OPS CHE
- [SDR CALA2025090108306](https://openairdocs.org/sdr/CALA2025090108306.md): Panel · corroded · Aug 29, 2025 · N657UA · Boeing 767322 · Fuselage Main, Structure
  > THERE IS CORROSION ON THE OVERWING FILL PORT CUTOUT OF THE RH WING. CLASSIFIED AS MAJOR REPAIR IAW GMM 03-20-20 AND RII AS PER GMM 09-25-05. REPAIRED THE CORROSION IAW EC/RA 5720-03551. ITEM OK TO SERVICE RT OVERWING FILL PORT CUTOUT WAS REPAIRED AND INSP
- [SDR CALA2025081407733](https://openairdocs.org/sdr/CALA2025081407733.md): Beam · corroded · Aug 12, 2025 · N657UA · Boeing 767322 · Cargo/Baggage Doors
  > FORWARD LARGE CARGO DOOR LOWER BEAM BS 562.4 - 575.6. ALL OF STEPS OF ECRA 5233-01037 WERE ACCOMPLISHED WITHOUT DEVIATION.
- [SDR CALA2025090108317](https://openairdocs.org/sdr/CALA2025090108317.md): Skin · damaged · Aug 11, 2025 · N657UA · Boeing 767322 · Fuselage Main, Structure
  > FWD DOOR 1L - FUSELAGE, SCRIBE LINES, GOUGES & DAMAGED FASTENER HOLES.. PERFORMED INTERIM REPAIR IAW EC/RA 5310-08669
- [SDR CALA2025090108316](https://openairdocs.org/sdr/CALA2025090108316.md): Failsafe · corroded · Aug 11, 2025 · N657UA · Boeing 767322 · Fuselage Main, Structure
  > FAIL-SAFE STRAP LOWER SURFACE CORROSION BETWEEN BS 1241 & 1263 MAJOR REPAIR AS PER GMM 03-20-20. PERFORMED INTERIM REPAIR AS PER EC/RA: 5360-01995. ALL THE STEPS OF THE EC/RA 5360-01995 HAVE BEEN INSPECTED. THIS REPAIR IS A PERMANENT SOLUTION WITH INSPECTION
- [SDR CALA2025090108315](https://openairdocs.org/sdr/CALA2025090108315.md): Skin · corroded · Aug 9, 2025 · N657UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > DURING LOWER LOBE INTERIOR BS 1540 TO 1629, CDP INSPECTION IT WAS FOUND SIGNS OF CORROSION ON SKIN BETWEEN S38L & S39L LOCATED BETWEEN BS 1540 & 1562. PERFORMED INTERIM REPAIR IAW EC/RA 5360-01993, REV A PERFORMED INSPECTION & INTERIM REPAIR WAS ACCOMPLIS
- [SDR CALA2025090108314](https://openairdocs.org/sdr/CALA2025090108314.md): Skin · cracked · Aug 9, 2025 · N657UA · Boeing 767322 · Service Doors
  > RIGHT FORWARD SERVICE DOOR AFT LOWER CORNER FASTENER HOLE CRACKED. PERFORMED INTERIM REPAIR IAW EC/RA: 5310-08664 ALL STEPS OF INTERIM REPAIR WERE ACCOMPLISHED AS PER EC/RA: 5310-08664 IT. IAW GMM 04-20-05 R1 FORWARD SERVICE DOOR AFT LOWER CORNER FASTENER H
- [SDR CALA2025041804023](https://openairdocs.org/sdr/CALA2025041804023.md): Turnbuckle · corroded · Apr 18, 2025 · N657UA · Boeing 767322 · Passenger/Crew Doors
  > L4 DOOR SLIDE REPLACEMENT. FOUND TURNBUCKLES ON FWD SIDE OF DOOR CORRODED. SEE PICS. CLEANED CORROSION IAW AMM 52-11-00-622-107. NO FURTHER DEFECTS NOTED. REAPPLIED CORROSION INHIBITING COMPOUND IAW AMM 51-24-09-377-008. OK TO CONTINUE
- [SDR CALA2025022602477](https://openairdocs.org/sdr/CALA2025022602477.md): Lens · missing · Feb 23, 2025 · N657UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHT OPPOSITE LAV B AT GALLEY STOWAGE 227F DAMAGED. EMERGENCY LIGHTING TESTED. ALL LIGHTS WORK BUT CLEAR PLASTIC COVER/LENS IS MISSING. REQUEST DEFERRAL PER MEL 3351C. FWD GALLEY LOWER WALL WHITE EMERGENCY AISLE LT INOP. DEFERRED PER MEL 3351C PART
- [SDR CALA2025022502468](https://openairdocs.org/sdr/CALA2025022502468.md): Fuel Sys · out of balance · Feb 22, 2025 · N657UA · Boeing 767322 · Aircraft Fuel Distribution System
  > FUEL CONFIG CAS IN CRZ. IMBALNCE OF 1900LBS. FM SUGGESTED POSS FUEL LEAK RTRNED TO LHR. CREW DEBRIEF C/OUT ON A/C RTN - REF MADE TO LP 3937863 - LEFT CTR FUEL PUMP INOP AS PER MEL 2822G. NIL FUEL LEAKS FOUND ON ARRIVAL. CREW BALANCED FUEL INBOUND, LEFT & RIG
- [SDR CALA2025010201744](https://openairdocs.org/sdr/CALA2025010201744.md): Unknown · odor · Dec 31, 2024 · N657UA · Boeing 767322 · Air Distribution System
  > ELECTRICAL SMELL IN CABIN FOLLOWING LIGHTNING STRIKE. CREW REPORTED SMELL IN FWD AND AFT GALLEY AREAS. RAN ENGINES AND PACKS WITH FLIGHT ENTERTAINMENT AND OTHER EQUIPMENT. FLIGHT AND CABIN CREW ON BOARD AND FOUND NO ODORS IN THE CABIN AT THIS TIME REF AMM 0
- [SDR CALA2024112702970](https://openairdocs.org/sdr/CALA2024112702970.md): Lens · missing · Nov 26, 2024 · N657UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY CEILING LIGHT IN FWD GALLEY ABOVE STOWAGE ZONE 200 LENS CAP IS MISSING. LENS REPLACED IAW AMM 33-51-04-002-001.
- [SDR CALA2024100700766](https://openairdocs.org/sdr/CALA2024100700766.md): Cable · misrouted · Oct 5, 2024 · N657UA · Boeing 767322 · Escape Slide
  > LEFT OFF WING SLIDE BOTTLE TRIGGER CABLE BALL FOUND BEHIND RETAINER CLIP TRIGGER CABLE ADJUSTED AS PER AMM 25-65-02-350-811-C2. BALL END NOW SAT CORRECTLY BEHIND THE RETAINER SPRING. RII REQUIRED AS PER GMM 09-25-05 CABLE TRIGGER BALL MECHANISM VERIFIED TO BE
- [SDR CALA2024080702177](https://openairdocs.org/sdr/CALA2024080702177.md): Skin · damaged · Jul 29, 2024 · N657UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT NR 2114213 WAS FOUND A DAMAGE ON FUSELAGE SKIN LH SIDE BETWEEN STA 1702 AND 1746.125, STRINGER 24L AND 26L. ITS NECESSARY TAKE ACTION TO PERFORM A REPAIR IAW SRM. TO PERFORM INSPECTION IAW SRM 53-00-01-2R-12 TABLE 202 & DELIVERY, REPEAT
- [SDR CALA2024070901978](https://openairdocs.org/sdr/CALA2024070901978.md): Transmitter · faulted · Jul 7, 2024 · N657UA · Boeing 767322 · Hydraulic Quantity Sensor
  > LOSS OF L HYD QTY WDM 29-33-11-2. RECONNECTED D38 AND REINSTALLED HYD MON UNIT. INSPECTED LT HYD QTY TRANSMITTER, SUSPECT TRANSMITTER AT FAULT. LT HYD QTY SHOWS 1.00 AT GATE. PERFORMED WIRE HARNESS SHAKEDOWN IAW WDM 29-33-11-2. ALL MEG CHECKED AND CONTINUIT
- [SDR CALA2024052001509](https://openairdocs.org/sdr/CALA2024052001509.md): Hose · leaking · May 18, 2024 · N657UA · Boeing 767322 · Crew Oxygen System
  > **CHRONIC LVL-2** DUE TO INCREASING FREQUENCY IN CREW O2 SERVICI NG WRITE-UPS, ACCOMPLISH THE FOLLOWING..1) PERFORM CREW O2 LEAK CHECK IAW AMM 35-11-00-795-106. PAY CLOSE ATTENTION TO ALL FITTI NGS AND PROPER STORAGE OF MASKS. LEAK WILL MOST LIKELY BE SMALL. R
- [SDR CALA2024043001276](https://openairdocs.org/sdr/CALA2024043001276.md): Steering Sys · malfunctioned · Apr 30, 2024 · N657UA · Boeing 767322 · Landing Gear Steering System
  > LOST NOSE WHEEL STEERING EXITING RUNWAY REF LOGPAGE 7815478 FOR X5 LANDING GEAR DOWNLOCK PIN INSTALLATION AS PART OF AIRCRAFT RETRIEVAL FROM TAXIWAY REF GMM 02-30-20 (2.C.(8)). GVI OF NLG PERFORMED. NIL SIGNS OF HYDRAULIC LEAKS AND STEERING CABLES CHECKED SECU
- [SDR CALA2024040400972](https://openairdocs.org/sdr/CALA2024040400972.md): Warning Message · false indication · Apr 4, 2024 · N657UA · Boeing 767322 · Central Warning
  > RUDDER RATIO EICAS AFTER TAKEOFF BRIEFED CREW; NO OVERWEIGHT LANDING,PILOT STATED PLANE FLEW FINE,JUST EICAS MSG AFTER TAKEOFF PERFORMED FIM TASK RUDDER RATION EICAS MSG 27-21 FAULT TREE PERFORMED YAW DAMPER SYSTEM BITE AS PER FIM 22-21 FAULT TREE 803 804.RU
- [SDR CALA2024031800760](https://openairdocs.org/sdr/CALA2024031800760.md): Lamp · failed · Mar 16, 2024 · N657UA · Boeing 767322 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - DOOR 1R EXTERIOR EMERGENCY LIGHT FAILED TO ILLUMINATE. LAMP REPLACED AS PER MM TASK 33-51-06-902-082 PARTS USED: 99-3351-3-0014,QTY:1
- [SDR CALA2024030600645](https://openairdocs.org/sdr/CALA2024030600645.md): Monitor · faulty · Mar 3, 2024 · N657UA · Boeing 767322 · Hydraulic Quantity Indicator
  > RT HYD QTY ON EICAS DURING TAKE OFF ROLL, EG RECOMMENDS PERFORMING B767 FIM TASK 29-11-00-211-802-C2 IN ORDER TO AID LOCATING THE HYD LEAK. REMOVED AND INSTALLED HYD RES TRANSMITTER ON THE RT RESERVOIR IN REVERENCE TO AMM TASK 29-33-02-004-001. REQUIRES HYD SE
- [SDR CALA2023101103030](https://openairdocs.org/sdr/CALA2023101103030.md): Nozzle · leaking · Sep 29, 2023 · N657UA · Boeing 767322 · Ice/Rain Protection System
  > OBSERVED SMOKE/STEAM COMING ACROSS CAPTAINS WINDOWS. 4 SEPERATE OCCURANCES. WX CLEAR. PERFORMED VISUAL CHECK OF TAT PROBE AS WELL AS FUNCTIONAL CHECK OF TAT PROBE HEAT REF AMM 30-33-00-715-010. TEST PASSED, NO DEFECTS NOTED. PERFORMED RAIN REPELLENT OPS CHECK
- [SDR CALA2023022200508](https://openairdocs.org/sdr/CALA2023022200508.md): Smoke Detector · none · Feb 21, 2023 · N657UA · Boeing 767322 · Fire Protection System
  > 2 HALON EXT USED FROM 1R AND 2R HALON EXTINGUISHERS (X2) USED NOT IN STOCK LHR, COMPLIED WITH 2 X HALON FIRE EXTINGUISHERS REQUIRED NIS LHR M&E REQUIREMENTS OF MEL 99-2626-3-0105, COMPLIED WITH REQUIREMENTS OF MEL. APPROVED
- [SDR CALA2022120803345](https://openairdocs.org/sdr/CALA2022120803345.md): Pump · failed · Dec 8, 2022 · N657UA · Boeing 767322 · Hydraulic Pump (Electric/Engine), Main
  > SUSPECT LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILURE. PUMP REPLACEMENT REQUIRED. REPLACED LEFT EDP PUMP ASSY IAW AMM 29-11-05-404-029-005 AND PUMP FAILED OPERATIONAL TEST. PERFORMED FIM 29-11 FAULT TREE 805 AND PER SHEET 2 BLOCK 27, SWAPPED OPERATIONAL PRESSURI
- [SDR CALA2022112103179](https://openairdocs.org/sdr/CALA2022112103179.md): Indicator · unserviceable · Nov 19, 2022 · N657UA · Boeing 767322 · Fuel Quantity Indicator
  > FUEL QTY IND EICAS S THE FQIS CANNOT ACCURATELY DETERMINE THE FUEL QUANTITY IN ONE OR MORE FUEL TANKS. R FUEL QTY INDICATOR INOP. NO TOTALIZER VALUE OVERHEAD OR IN FM C ALSO. LOCK FOR POSITIVE FIX, ALSO HISTORY ON LP 3083170 15NOV22 UNLOCKED TO CLEAR REFERENC
- [SDR CALA2022091902417](https://openairdocs.org/sdr/CALA2022091902417.md): Door · stuck · Sep 19, 2022 · N657UA · Boeing 767 · Doors
  > FWD ENTRY DOOR WILL NOT RETRACT OPEN DO TO INSIDE FOLDING CEILING PANEL OUT OF SEQUENCE REF AAR N/R 9029568 INSTALLED MISSING BOLT ON OVERCENTER MECHANISM LATCH TUBE.
- [SDR CALA2022061701522](https://openairdocs.org/sdr/CALA2022061701522.md): Floorbeam · cracked · Jun 16, 2022 · N657UA · Boeing 767322 · Fuselage Main, Floor Beam
  > B767-53-3-7002, CABIN- STA 287, RBL 80 AREA FLOORBEAM FOUND CRACKED TRANSFER REF HXWO 821634 AND ORIGINATED BY EMP V897790 CABIN STA287 RBL33.5 TO RBL82 AREA FLOORBEAM REPAIRED AS PER ECRA5320-02964 REV - ATTACH FORM 44-0008 WORKSHEET ITEM 1 TO ITEM36 ACCOMPLI
- [SDR CALA2022061701521](https://openairdocs.org/sdr/CALA2022061701521.md): Floorbeam · corroded · Jun 16, 2022 · N657UA · Boeing 767322 · Fuselage Structure (General)
  > B767-53-3-7002 CABIN STA303 LBL24 TO 54 FLOORBEAM FOUND CORROSION TRANSFER REF HXWO 822811 AND ORIGINATED BY EMP V897790 CABIN STA303 LBL46" TO LBL54" FLOOR EAM CORROSION BLEND OUT REPAIR 1 FIG.201 ATTACH FORM 44-0008 WORKSHEET ITEM 1 TO ITEM33 AREA REMAIN 0.0
- [SDR CALA2021052600735](https://openairdocs.org/sdr/CALA2021052600735.md): Skin · cracked · May 25, 2021 · N657UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > B767-53-3-7064 - LOWER HALF FUSELAGE STA 1438 BETWEEN S38R-S39R HAS CRACK REF NRC 9130394, SKIN DAMAGED AREA TRIMMED OFF PER SRM 53-00-01- 2R-29 REAPIR FIG 201. SKIN THICKNESS IS 0.056". HFEC CARRIED OUT PER B767 NTM PART6 51-00-19 REV 125, NO CRACK FOUND. REP
- [SDR CALA2020011000118](https://openairdocs.org/sdr/CALA2020011000118.md): Sensor · faulty · Jan 9, 2020 · N657UA · Boeing 767322 · Leading Edge Slat Position Indicating System
  > LEADING EDGE SLAT SYSTEM ALTERNATE LEADING EDGE SLATS PROBLEM WAS ENCOUNTERED BY THE FLIGHT CREW WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS. LE SLAT ASYM EICAS MSG DURING FLT LE SLAT ASYM EICAS ALSO ON FINAL. PER TECH SUPPORT FOUND PSEU FAULT WITH PROX SE
- [SDR CALA2019110501924](https://openairdocs.org/sdr/CALA2019110501924.md): Connector · defective · Nov 4, 2019 · N657UA · Boeing 767322 · Hydraulic Power System Wiring
  > HYD SYS PRESS -R INTERMITTENT EICAS ALONG WITH FLICKERING BRAKE SOURCE LIGHT(INTERMITTENT. NEED POSITIVE FIX UNLOCK UNLOCKED DEBRIEFED CREW: PILOT REPORTED THAT THEY NOTICED THIS ISSUE AFTER THEY REACHED CRUISE ALTITUDE. PILOT SAW THE BRAKE SOURCE LIGHT FLIC
- [SDR CALA2019110301895](https://openairdocs.org/sdr/CALA2019110301895.md): Pump · failed · Oct 31, 2019 · N657UA · Boeing 767322 · Hydraulic Pump (Electric/Engine), Main
  > WITH THE R ELEC HYD PUMP ON/R LOW PRESSURE SYS. AND BRAKE SOURCE LIGHT CAME ON/FOLLOW QRH. ACMP SHOWS FLUCTUATIONS IN PRESSURE WHEN A LOAD WAS APPLIED. REMOVED ACMP IAW AMM 29-11-01-024-001 AND ORDERED REPLACEMENT VIBRATION MOUNTS AND HARDWARE. REPLACED RIGHT
- [SDR CALA2019101401756](https://openairdocs.org/sdr/CALA2019101401756.md): Pressure Switch · inoperative · Oct 14, 2019 · N657UA · Boeing 767322 · Hydraulic Pressure Regulator, Main
  > HYD SYS PRESS R EICAS CAUTION CAME ON IN FLIGHT DEBRIEF CREW RIGHT ELEC PRESS LIGHT FLICKERED AND SYS PRESS LIGH T ILLUMINATED. R ENG HYD PUMP TURNED OFF AND RIGHT ELEC LEFT ON STILL HAD SYS PRESS LIGHT ILLUMINATED. RAN RIGHT ENG FOR 5 MINUT ES NO FAULTS NOTED
- [SDR CALA2019100501696](https://openairdocs.org/sdr/CALA2019100501696.md): Stringer · cracked · Oct 2, 2019 · N657UA · Boeing 767322 · Fuselage Main, Longeron/Stringer
  > SUPPORT TASK - FX STA1439-1461 STR24R FOUND CRACKED AND PREVIOUS LY REPAIRED (AFTER SKIN DOUBLER REMOVED).REF NR LP 9132054 FX STA1417 TO STA1486 STR24R REPAIRED AS PER ECRA 5331-02466 REV - PART 1 ITEM 1 (STRINGER REPAIR IN CATEGORY A REPAIR) AND SKIN REPAIRE
- [SDR CALA2019101101745](https://openairdocs.org/sdr/CALA2019101101745.md): Skin · cracked · Oct 1, 2019 · N657UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > SUPPORT TASK TAR - QC PICK UP SHEET - EXTERNAL FUSELAGE REPAIR NOT LISTED FOR INSPECTION FROM AIRCRAFT RECORD BTN BS1605-1629 LWR FUSELAGE RBL 6".PLS ADV REPAIR RECORD OR REPAIR INSTRUCTION REF TO NR LP:9131989 BS 1605-29 REPAIRED IAW ECRA 5331-02462 AND SRM 5
- [SDR CALA2019100501692](https://openairdocs.org/sdr/CALA2019100501692.md): Frame · corroded · Oct 1, 2019 · N657UA · Boeing 767322 · Fuselage Main, Frame
  > B767-53-3-7035 CABIN STA 977 R/H FRAME LWR CORNER FOUND CORRODED REF TO NR LP:9131109 RH FRAME STA 977 CORROSION REPAIRED IAW ECRA 5311-02261. THIS IS A DAMAGE TOLERANCE REPAIR IAW SRM 53-00-06, CAT C, AND REQUIRES REPLACEMENT WITHIN 24 MONTHS OR 3,OOO FC, WHI
- [SDR CALA2019100501691](https://openairdocs.org/sdr/CALA2019100501691.md): Skin · dented · Oct 1, 2019 · N657UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > SUPPORT TASK TAR - LP 6587012 FUSELAGE SKIN DENT BETWEEN STA355 AND STA368 S-22R TO S-23R AFTER MEASURED OF THE DENT, THE DEPTH IS 0.119" LENGTH IS 3.2" AND WIDTH IS 2.1".A/Y IS LESS THAN 30 OUT OF LIMITS AS PER SRM 53-00-01 ALLOWABLE DAMAGE 1, NO APPLICABLE R
- [SDR CALA2019100541683](https://openairdocs.org/sdr/CALA2019100541683.md): Skin · dented · Sep 30, 2019 · N657UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > BS 1417-1486, STR 24R DENT REPAIRED IAW ECRA 5331-02466, REF ELB LP 3408629 AND HAECO NR LP 9132054, DURING HKG 2C VISIT. ECRA 5331-02466 PART 2 REQUIRES INSPECTION ON OR BEFORE 37,500 FC AND REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,000 FC. IAW ECRA 53
- [SDR CALA2019092801655](https://openairdocs.org/sdr/CALA2019092801655.md): Attach Angle · damaged · Sep 26, 2019 · N657UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > SUPPORT TASK QC PICK UP SHEET - TOOLING MARKS LOCATED ON ATTACH ANGLE AT STA977 AT STRINGER 22L,WL180,ON TOP OF PRESSURE DECK CAUSED BY LEVELING COMPOUND REMOVAL.REF NR LP 9131376 CABIN STA977 S22L PRESSURE DECK LUB ATTACH ANGLE REPLACED AS PER SRM 51-10-02 AN
- [SDR CALA2019092801654](https://openairdocs.org/sdr/CALA2019092801654.md): Floorbeam · corroded · Sep 26, 2019 · N657UA · Boeing 767322 · Fuselage Main, Floor Beam
  > B767-53-3-7154 - AFT CGO COMPT L/H TORQUE BOX PNL SUPPORT BOTTOM AREA FOUND CORROSION STA 1285 LBL9-24 FLOOR BEAM AREA.REF TO NR LP:9131604 AFT CGO LH TORQUE BOX PANEL SUPPORT STA1285 LBL40-RBL40 FLOOR BE AM REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED
- [SDR CALA2019092801653](https://openairdocs.org/sdr/CALA2019092801653.md): Attach Angle · damaged · Sep 26, 2019 · N657UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > SUPPORT TASK QC PICK UP SHEET - TOOLING MARKS LOCATED ON ATTACH ANGLE AT STA977 AT STR 22R,WL180,ON TOP OF PRESSURE DECK CAUSED BY LEVELING COMPOUND REMOVAL.REF NR LP 9131377 CABIN STA977 STR22R WL180 ANGLE REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED A
- [SDR CALA2019092801645](https://openairdocs.org/sdr/CALA2019092801645.md): Frame · corroded · Sep 25, 2019 · N657UA · Boeing 767322 · Fuselage Main, Frame
  > B767-53-3-7035 CABIN STA 977 L/H FRAME LWR CORNER FOUND CORRODED REFER TO NR LP:9131108 CABIN STA 977 L/H FRAME OUTER CHORD REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 JUST BETWEEN STR-8L AND STR-22AL NEW CHORD P/N:145T1062-35 GRN H19S244823
- [SDR CALA2019092801647](https://openairdocs.org/sdr/CALA2019092801647.md): Skin · not reported · Sep 25, 2019 · N657UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > REFERENCE LP#3339628 S/M REPAIR OVER DOOR 1L. REPAIR WAS PREFORM ED PER SRM53-00-01 REPAIR 12. DIP IS REQUIRED FOR REINSPECT. FIR ST REINSPECT IS 6,000 F/C AFTER REPAIR & REPEAT INSP EVERY 9,000 F/C REFERENCE SRM 53-00-01 REPAIR 12 TABLE 202. DIP REQUESTED FOR
- [SDR CALA2019050300690](https://openairdocs.org/sdr/CALA2019050300690.md): Wire · damaged · May 3, 2019 · N657UA · Boeing 767322 · Equipment/Furnishings Wiring
  > DURING CLIMB PAX SAW A FLASH ABOVE ROW 20 FOLLOWED BY SMOKE AND FUMES. REF AMM05-51-56 SMOKE INSPECTION. REMOVED CABIN CEILING PANELS AT 19-20 ABC AND 19-20 KL. CONFIRMED HEAT DAMAGE ON LEFT SIDE CEILING BETWEEN STATION 764 AND 808 REQUIRING FURTHER INVESTIGAT

Next page: https://openairdocs.org/aircraft/N657UA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N657UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N657UA/reports

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